z. .. - ‘ gages , . V .-...,.i......5 . V _ . . £34.. ,3. . V Ln. .. r . , , . . ‘ .43.“. . , V . .......:.m...,.V V V ,2 ‘ . 5% . . . 34...? V .? 7 3 Pariiukv 7:. 1.5 .:2.... in. i. 0.. ‘ . .HA 9....ny .52.... h a. Mars. r . x V t {.43.} ...r18 .1... .Il... 5.1.53. .a:..1:.. ..I.. . Oahu-:5 hunk... 3 .. an...) I .3111... 1.1%.}, .2... ..!.171.. 4.9.x ‘ 4.2.9... . I.\v:t c. . 3.x: .1. . 4.5.5.151. .‘Ittvil .31..»11 .2. A, r. .9. .- .JVMF .2 v5 {1... . I 3 . A . , I \ 3. g. . R. : «:4 P159; . , V . V a .V. ‘ n V V .nmw V9.9.) 1...: :1... . , . ‘ ‘ V. :i llllUllllUHIIHHUW:IUIHHHII‘JUIIWHHIIIIUW 193 01046 3473 This is to certify that the dissertation entitled Evaluation of Hydraulic Controls to Promote Surfactant Dissolution of Trapped Residual NAPL presented by Lizette Rita Chevalier has been accepted towards fulfillment of the requirements for Ph . D . degree in Civil Engineering QM W%M ._ Major profes’ / Date October, 1994 / CL-Mbjor Professor MS U is an Affirmative Action/Equal Opportunity Institution 0-12771 LIBRARY Mlchlgan State University PLACE IN RETURN BOX to move this Mutton mm ' To AVOID FINES return on or before due date . DATE DUE DATE DUE DATE DUE EVALUATION OF HYDRAULIC CONTROLS TO PROMOTE SURFACTANT DISSOLUTION OF TRAPPED RESIDUAL NAPL By Lizette Rita Chevalier A DISSERTATION Submitted to Michigan State University in partial fialfillment of the requirements for the degree of DOCTOR OF PHILOSOPHY Department of Civil and Environmental Engineering 1 994 ABSTRACT EVALUATION OF HYDRAULIC CONTROLS TO PROMOTE SURFACTANT ENHANCED DISSOLUTION OF TRAPPED RESIDUAL NAPL by Lizette Rita Chevalier Hydraulic controls to deliver, recover and promote the efiicient use of aqueous phase surfactants to enhance the dissolution of trapped residual non-aqueous phase liquids near the water table were investigated through experiments and numerical modeling. Soil column experiments were designed to simulate conditions near the capillary fiinge where a non-aqueous phase liquid may become trapped as a discontinuous immobile phase. A lumped mass transfer coefiicient for the dissolution of dodecane into a surfactant enhanced aqueous phase was measured in a flow interruption study which determined that the mass transfer is rate limited, but not prohibitively slow. Experiments were conducted to measured the reduced relative permeability of the aqueous phase as a fimction of saturation in a natural unconsolidated porous media where a trapped residual nonwetting phase increases the resistance to aqueous flow. The data presented includes an experiment where the trapped residual nonwetting phase was reduced through surfactant enhanced dissolution in addition to measurements with a trapped residual intermediate wetting phase present. An analytical technique was developed to measure the concentration of dodecane in a surfactant using head space gas chromatography which overcomes the effects of surfactant concentration on the degree of partitioning between the gaseous and aqueous phase. An implicit l-D transport code was developed to estimate the surfactant enhanced dissolution of a uniform saturation of trapped residual non-aqueous phase. Graphs are presented using dimensionless parameters to predict the time required for remediation and to select a pumping rate promoting a high concentration of the contaminant while minimizing the generation of waste water. A two-dimensional study was conducted in a laboratory scale model aquifer using the United States Geological Survey model SUTRA, a finite element code for saturated and unsaturated flow with contaminant transport. The efficiency of the hydraulic systems was based on delivering the surfactant throughout the contaminated region, ensuring sufficient contact time between the surfactant and the contaminated region, and recovering contaminant laden surfactant enhanced ground water. The results of the research show the promising potential and the need for further research in surfactant enhanced pump-and-treat methods to remediate aquifers contaminated with trapped residual non-aqueous phase liquids. I dedicate this work, and the future work I do in the remediation of the earth and her waters to the friends who died of cancer during the time I conducted this research ~ Joyce Laderman, Helen Catherino and James Boggs. iv Acknowledgments In respect, I would first like to thank my advisors Dr. David C. Wiggert and Dr. Roger E. Wallace for their support, advice and criticism of my research. I would also like to extend my appreciation to the other two members of my committee, Dr. Susan J. Masten of the Department of Civil and Environmental Engineering and Dr. Raymond J. Kunze of the Department of Crop and Soil Sciences for their advice and encouragement. I would also like to thank Dr. Thomas Voice and Dr. Paul Loconto for their assistance. I am grateful for the research funding provided by the US. Environmental Protection Agency Ofice of Research and Development under a grant to the Great Lakes and Mid-Atlantic Hazardous Substance Research Center. I would also like to thank the College of Engineering at Michigan State University for the support received through the Dean‘s Distinguished Fellowship. I also appreciate the support I received through a General Electric Graduate Fellowship and an internship at General Motors NAO Research and Development Center under the guidance of Dr. Abdul S. Abdul. On the personal side, I gratefully thank my mother and proof-reader, Irene A. Chevalier as well as my father, Leo N. Chevalier, for their encouragement and pride. I appreciate the friendship and endless hours of conversation shared with many of my colleagues, especially Herr Soeryantono, Reza Rakhshandehroo, Sashi Nair, Munjed Maraqa and Jehng-Jyun (J .J .) Yao, all of which certainly enhanced the time spent at MSU. My sincere thanks and love for the support and continued encouragement from the Women in my life ~ Christine Reagan-Rosales, Ann Perrault, Sharon Howell, Sherry Hon, Lucinda Lehmkuhle, Leah Cohen and most importantly, Lynette J. Holloway. Table of Contents List of Tables .................................................................................................................. ix List of Figures ................................................................................................................. x Nomenclature ............................................................................................................... xvi Chapter 1. Introduction 1.1 Problem Statement ......................................................................................... 1 1.2 Objective and Scope of the Research .............................................................. 3 Chapter 2. Background 2.1 Irnmiscible Fluids at the Pore Scale ................................................................. 6 2.2 NAPL Entrapment as a Discontinuous Residual Phase .................................... 7 2.3 Hydraulic Conductivity and Permeability ........................................................ 8 2.4 Mobilization of Trapped Residual NAPL ...................................................... 10 2.5 Surfactants ................................................................................................... 13 2.6 Kinetics of Surfactant Enhanced Dissolution ................................................. 14 2.7 Surfactant Transport of Dissolved NAPL ..................................................... 15 Chapter 3. Materials and Methods 3.1 Apparatus .................................................................................................... 23 3.2 Preparation of Soil Column .......................................................................... 24 3.3 Establishing a Trapped Residual Irnmiscible Phase ........................................ 24 3.4 Hydraulic Conductivity Measurements ......................................................... 26 3.5 Equilibrium Solubility of NAPL in Surfactant ............................................... 27 3 .6 Investigation of the Kinetics of Surfactant Enhanced Dissolution of Trapped Residual NAPL .................................................................... 27 3.7 Dye Sorption Measurements ........................................................................ 28 3.8 Error Analysis .............................................................................................. 28 3.9 Material ....................................................................................................... 29 Chapter IV. Column Experiments in Surfactant Enhanced Dissolution of Trapped Residual Dodecane 4.1 Introduction ................................................................................................. 35 4.2 Objective ...................................................................................................... 37 vii 4.3 Background ................................................................................................. 37 4.4 Apparatus and Materials ............................................................................... 41 4.5 Methods ....................................................................................................... 41 4.6 Results and Discussion ................................................................................. 43 4.6.1 Analytical Method ............................................................................... 43 4.6.2 Equilibrium Solubility .......................................................................... 45 4.6.3 Kinetics of Dodecane Dissolution ........................................................ 46 4.6.4 Breakthrough Curve ............................................................................ 48 4.6.5 Long Term Continuous Pumping ......................................................... 50 4.7 Summary ...................................................................................................... 51 Chapter V. Aqueous Permeability Prior to and During Surfactant Enhanced Dissolution of Trapped Residual NAPL 5.1 Introduction ................................................................................................. 59 5.2 Materials and Methods ................................................................................. 62 5.3 Results and Discussion ................................................................................. 64 5.3.1 Trapped Residual NAPL ...................................................................... 65 5.3.2 Reduced Permeability Of the Aqueous Phase Due to Trapped Residual Phases ................................................................................... 68 5.3.3 Aqueous Phase Permeability During Surfactant Enhanced Dissolution of NAPL ........................................................................... 69 5.3.4 Comparing Data in Discontinuous Region with Existing Fitting Parameters .......................................................................................... 70 5.4 Summary ...................................................................................................... 72 Chapter VI. Numerical Modeling 6.1 Introduction ................................................................................................. 86 6.2 Objective ...................................................................................................... 89 6.3 One Dimensional Model Development .......................................................... 90 6.4 Simulation Studies Using l-D Implicit Transport Model ............................... 95 6.5 Verification of 2-D Numerical Code ............................................................. 98 6.6 Two Dimensional Model Simulations ......................................................... 101 6.7 Summary .................................................................................................... 108 Chapter VII. Dissertation Summary and Recommendations 7.1 Summary .................................................................................................... 147 7.2 Summary of Costs ...................................................................................... 152 7.2 Recommendations ...................................................................................... 152 Appendix A: Analytical Solution to the 1-D Transport Equation ................................. 155 Appendix B: ID Code for Surfactant Enhanced Dissolution of an Irnmobile Residual NAPL ............................................................................ 156 Appendix C: Determination of Mass Transfer Coefficient: Output fiom SCIENTIST Software .................................................................. 162 viii Appendix D:Summary of Input Data used in SUTRA Model ........................................ 165 Appendix B: Materials and Suppliers ........................................................................... 169 List of References ........................................................................................................ 164 Table 2.1 Table 3.1 Table 4.1 Table 4.2 Table 5.1 Table 5.2 Table 5.3 Table 5.4 Table 6.1 Table 6.2 Table 6.3 Table 6.4 Table 7.1 Table C1.1 Table C1.2 Table D1,] List of Tables Overview of past research in NAPL entrapment and mobilization ........... 22 Fluid properties of dodecane ................................................................... 34 GC settings ............................................................................................. 58 Experimental set-up for breakthrough curves .......................................... 58 Capillary number vs. saturation ............................................................... 82 Soil and fluid properties .......................................................................... 83 Order of magnitude estimate for ganglia size ........................................... 84 Reported values of fitting parameters for white Ottawa sand used in relative permeability-saturation and capillary pressure-saturation relationships in a 2-phase system ............................................................. 85 Soil and fluid properties used in model simulations ............................... 144 Representative range of mass transfer coefficients ................................. 144 Error propagation for lumped mass transfer coefficient (k1), saturatation of trapped residual NAPL (Sm). and dispersivity (or) ..................................................................................... 145 Summary of well schemes for evaluation of hydraulic controls .............. 146 Summary of costs in 1986 dollars involved with in-situ leaching (Roy F. Weston, Inc. 1988) .................................................................. 154 Output from Scientist Software used to determine mass transfer coefficient, k1= 0.387 hrl. ................................................................... 162 Output from Scientist Software used to determine mass transfer coefficient, k1= 0.161 hrl. ................................................................... 164 Data used in SUTRA numerical simulations .......................................... 165 Figure 1.1 Figure 2.1 Figure 2.2 Figure 2.3 Figure 2.4 Figure 2.5 Figure 2.6 Figure 2.7 Figure 2.8 Figure 3.1 Figure 3.2 Figure 3.3 Figure 3.4 List of Figures Schematic of an unconfined aquifer with LNAPL and DNAPL spills ..................................................................................... 5 Schematic of pore space characteristics ................................................... 17 Pressure difl‘erence at the interface of immiscible fluids in an idealized pore throat or pore body ......................................................................... 18 Relative effect of the capillary number as a function of trapped residual saturation at Bond numbers less than 0.00667 (adapted from Morrow and Songkran 1981) ........................................... 18 Relative permeability as a function of phase saturation ............................ 19 Flow passing through a permeable cylinder in a uniform flow field relative to the flow passing through a cylinder when k, = 1 (adapted from Wheatcrafi and Winterberg 1985) ................................................... 19 Relative correlation of the mobilization of residual oil and capillary number for uniform glass beads (adapted from Morrow et al. 1988) .................... 20 Schematic of a surfactant micelle capturing and idealized NAPL ganglia. 20 Relative changes in physical properties in the neighborhood of the critical micelle concentration (adapted fi'om Preston 1948) ..................... 21 1-D column ............................................................................................ 31 Schematic of apparatus used to conduct falling head hydraulic conductivity measurements ..................................................................... 32 General schematic of apparatus used to measure hydraulic conductivity ased on the head difi‘erence across the column ..................... 32 Grain size distribution of white Ottawa sand ........................................... 33 Figure 3.5 Figure 4.1 Figure 4.2 Figure 4.3 Figure 4.4 Figure 4.5 Figure 4.6 Figure 4.7 Figure 4.8 Figure 4.9 Figure 4.10 Figure 4.11 Figure 4.12 Figure 5.1 Figure 5.2 Figure 5.3 Adsorption isotherm for Red-O dye ........................................................ 33 GC response to dodecane concentration at varying surfactant concentration illustrating the effects of surfactant concentration on partitioning of dodecane .................................................................... 52 GC measurement of 4 ppm dodecane in varying surfactant concentration with salt ............................................................................ 52 7 Four ppm undecane at varying surfactant concentrations ......................... 53 The influence of thermostat temperature and equilibrium time (temp/time) on calibration curves ............................................................................... 53 Equilibrium solubility for dodecane for varying concentrations of Witconol NP-150. .................................................................................. 54 Critical micelle concentration of Witconol NP-l 50 determined from surface tension (Witco 1991) .................................................................. 54 Flow interruption study. ......................................................................... 55 Error associated with enhanced solubility measurement in flow interruption study ................................................................................... 55 Continuous pumping of Witconol NP-l 50 followed by a water flush and subsequent pulsed pumping .............................................................. 56 Breakthrough curves for 5% Mtconol NP-150 injected into regions of trapped residual dodecane .................................................................. 56 Error associated with break through curves ............................................ 57 Compilation of breakthrough curves ....................................................... 57 Measured values of permeability-saturation for trapped residual air and trapped residual NAPL ..................................................................... 75 Aqueous phase relative permeability as trapped residual NAPL is reduced through surfactant enhanced dissolution .................................................. 76 Error associated with aqueous phase relative permeability measurements. 76 xii Figure 5.4 Comparing data to Corey and van Genuchten equations for the relative permeability-saturation relationship of the aqueous phase with a residual aqueous phase saturation of 0.093 (A = 2.30, n' = 1.55) ............................................................................................... 77 Figure 5.5 Comparing data to Corey and van Genuchten equations for the relative permeability-saturation relationship of the aqueous phase with a residual aqueous phase saturation of 0.093 (it = 2.32, n' = 4.27) ............................................................................................... 78 Figure 5.6 Comparing data to Corey and van Genuchten equations for the relative permeability-saturation relationship of the aqueous phase with a residual aqueous phase saturation of 0.093 (X = 2.34, n' = 6.99) ............................................................................................... 79 Figure 5.7 Comparing data to Corey and van Genuchten equations for the relative permeability-saturation relationship of the aqueous phase with a residual aqueous phase saturation of 0.093 (A = 2.30, n '= 3.58) ................................................................................................ 80 Figure 5.8 Comparing data to Corey and van Genuchten equations for the relative permeability-saturation relationship of the aqueous phase with a residual aqueous phase saturation of 0.093 (A = 3.46, n '= 7.42) ................................................................................................ 81 Figure 6.1 Implicit numerical solution compared to analytical solution (Cr=0.5;L=15cm;ro=0.5;Da =1;Ax=0.5cm) ........................... 111 Figure 6.2 Maximum and minimum relative error over a range of velocities as indicated by the range ofDa (Cr = 0.3; L = 15 cm; 0) = 0.6; Ax = 1 cm). ........................................................................................ 111 Figure 6.3 Summary of study to optimize the Courant number over a rangeofrovalues(L=15cm;Ar=1cm). ............................................ 112 Figure 6.4 Relative error over a range of Da numbers represented in previous table (Cr = 0.3; (0 = 0.6; Q = 0.5 mllmin; . L=15cm;Ax=1cm) .......................................................................... 112 Figure 6.5 Relative error over a range of Pa numbers (Cr = 0.3; a) = 0.6; Q=0.5ml/min;L=15cm;Ax=lcm) ................................................ 113 Figure 6.6 Figure 6.7 Figure 6.8 Figure 6.9 Figure 6.10 Figure 6.11 Figure 6.12 Figure 6.13 Figure 6.14 Figure 6.15. Figure 6.16 Figure 6.17 Figure 6.18 Figure 6.19 Figure 6.20 xiii Fraction of trapped residual NAPL remaining in pores spaces over the length of the column over time (Da=10,Cr= 0.3;co=0.6;L=15cm;Ax=1cm) ............................ 113 Dimensionless analysis of surfactant enhanced dissolution of trapped residual dodecane (Da = 1,Cr = 0.3; co = 0.6; L=15cm;Ax=1cm) .......................................................................... 114 Dimensionless analysis of surfactant enhanced dissolution of trapped residual dodecane (Da = 100,Cr = 0.3; 0) = 0.6; L=15cm;Ax=lcm) .......................................................................... 114 Rate-limited dissolution of NAPL into surfactant enhanced aqueous phase ...................................................................................... 115 Normalized effluent concentrations over a range of Da ......................... 115 Comparing eflluent concentrations when velocity is determined from total porosity, effective porosity and variable effective porosity ................................................................................................ 116 Experimental and implicit modeled effluent concentrations of dodecane in a 5% nonionic surfactant enhanced aqueous phase ............. 116 Pores volumes needed to reach MCL over a range of Damkohler numbers .............................................................................. 117 Model aquifer region. ........................................................................... 118 Elements in the saturated/unsaturated grid ............................................ 119 Nodes in the Saturated/Unsaturated grid ............................................... 120 Pressure-saturation relationship based on van Genuchten parameters 121 Schematic illustration of the water table and boundary conditions for analytical solution of seepage through a dam (based on Wang and Anderson 1979) .................................................................................... 121 Results of the comparison of SUTRA with analytical solution for determining the surfact of the watertable through the aquifer ................ 122 Comparison of numerical and anlytical solution for transport of an instantaneous point source .................................................................... 122 Figure 6.21 Figure 6.22 Figure 6.23 Figure 6.24 Figure 6.25 Figure 6.26 Figure 6.27 Figure 6.28 Figure 6.29 Figure 6.30 Figure 6.31 Figure 6.32 Figure 6.33 Figure 6.34 Figure 6.35 Figure 6.36 Figure 6.37 Figure 6.38 Figure 6.39 xiv Geometry used in evaluation of well placement ..................................... 123 Concentration profiles as plume migrates through a region of contamination where the relative permeability and effective porosity are reduced due to trapped residual NAPL (Case 1a) at t=1.67 hr, 3.4 hr, and 5 hr. ................................................................ 124 Concentration profiles as plume migrates through a homogeneous medium (Case 1b) at t=1.67 hr, 3.4 hr, and 5 hr. ................................... 125 Summary of 5% concentration profile at 5 hours for Case 1a and Case 1b ................................................................................................ 126 Velocity vector plot for Case 9 (Table 6.4) ........................................... 127 Velocity vector plot for Case 8 (Table 6.4) ........................................... 128 Velocity vector plot for Case 1a (Table 6.4) ......................................... 129 Velocity vector plot for Case 1b (Table 6.4) ......................................... 130 Concentration contour plot for Case 2 (Table 6.4) ................................ 131 Velocity vector plot for Case 2 (Table 6.4) ........................................... 132 Fraction of mass removed in each region after surfactant flushing 60 pore volumes ................................................................................... 133 Concentration contour plot for Case 3 (Table 6.4) ................................ 134 Velocity vector plot for Case 3 (Table 6.4) ........................................... 135 Concentration contour plot for Case 4 (Table 6.4) ................................ 136 Velocity vector plot for Case 4 (Table 6.4) ........................................... 137 Concentration contour plot for Case 5 (Table 6.4) ................................ 138 Velocity vector plot for Case 5 (Table 6.4) ........................................... 139 Concentration contour plot for Case 6 (Table 6.4) ................................ 140 Velocity vector plot for Case 6 (Table 6.4) ........................................... 141 Figure 6.40 Concentration contour plot for Case 7 (Table 6.4) ................................ 142 Figure 6.41 Velocity vector plot for Case 7 (Table 6.4) ........................................... 143 Nomenclature A .................... cross sectional area of soil, L2 a ..................... cross sectional area of standpipe, L2 b ..................... width, L C .................... aqueous phase solute concentration, ML’3 Cr ................... Courant number (dimensionless) C s ................... aqueous phase equilibrium solute concentration, M];3 C“, ............... aqueous phase surfactant concentration, ML“3 c,- .................... distance from upper region of contaminated plume to well, L D .................... hydrodynamic dispersion coefficient, L2T'l D“ .................. coefficient of molecular difl’usion, LZT'1 Da .................. Damkohler number (dimensionless) D, ................... fi'ee liquid difl‘usivity of the solute, L2T'l d ..................... grain diameter, L d, .................... distance from center of contaminated plume to well, L Fa, ................. fraction of flow reduced (dimensionless) F g ................... gravity forces, MLT"2 F r ................... interfacial tension forces, MLT'2 Fv ................... viscous forces, MLT'2 g ..................... gravitational constant, LT'2 Hi ................... hydraulic head, L i ..................... hydraulic gradient (dimensionless) J ..................... flux of mass across interface, ML'ZT'1 K .................... hydraulic conductivity, LT'l k ..................... permeability, L2 k, .................... lumped mass transfer coefficient, LT‘l I ..................... characteristic length, L L .................... length of column, L Ly ................... vertical length of ganglia, L L}, .................. horizontal length of ganglia, L m .................... fitting parameter M ................... mass, M MC .................. column mass, M Md .................. dry mass of packed soil column, M MW ................. mass of water in soil column, M we ................. mobility ratio" (dimensionless) n ..................... porosity (dimensionless) n' .................... fitting parameter Nb .................. bond number (dimensionless) Nc .................. capillary number (dimensionless) P .................... pressure, ML'lT'2 PC ................... capillary pressure, ML'lT'2 Pe .................. Péchlet number (dimensionless) PV .................. pore volume, L3 PV" ................ aqueous phase pore volume after trapped residual NAPL, L3 PV; ................. initial pore volume, L3 Q .................... flow, L3 T"1 Q; ................... scaled source/sink (dimensionless) Qa .................. flux through contaminated region R .................... grain radius, L 82 .................. uncertainty interval (residual error) Re .................. Reynolds number (dimensionless) S ..................... saturation (dimensionless) s», ................. standard error of the y estimate 1 ..................... time, T 1w,” ............ Student’s t t" .................... dimensionless time, pore volume v ..................... average pore velocity, LT“l Vc ................... volume of column, L3 Va,p ................ volume in column caps, L3 w .................... width of contaminated region, L x} ................... scaled x—distance fi'om centerline of contaminated region (dimensionless) x,- .................... Cartesian coordinates, L y',- ................... scales y-distance from top of contaminated region (dimensionless) y ..................... Cartesian coordinates, L xviii z ..................... elevation head, L Greek p .................... density, ML'3 A .................... difference a .................... dispersivity, L a' .................... fitting parameter A. .................... fitting parameter (a .................... implicit weighting parameter a .................... interfacial tension, ML‘ZT'2 e ..................... relative error t ..................... stress, ML'IT'2 6 ..................... thickness of stagnant film layer, L if .................... viscosity, ML‘IT'l Subscripts a ..................... aqueous phase b ..................... bulk e ..................... effective g ..................... gaseous phase ma .................. maximum aqueous phase It ..................... NAPL mv .................. nonwetting p ..................... phase r ..................... relative ra ................... irreducible aqueous phase rg ................... trapped residual gaseous (air) phase rn ................... trapped residual NAPL (oil) phase s ..................... saturated w .................... wetting Chapter 1 Introduction 1.1 Problem Statement Surface spills, tank leaks and improper disposal practices may result in aquifer contamination by a pollutant immiscible with the groundwater, such as gasoline. As the volume of nonaqueous phase liquid (N APL) advances under the influence of gravity through the porous matrix, a residual volume will remain in the pores, trapped by capillary forces. In the upper region of an unconfined aquifer, the NAPL will migrate through pores initially saturated with a continuous aqueous and gaseous phase, referred to as the vadose zone (Fig. 1.1). In this region, as much as 9% of a pore space will become occupied with residual NAPL (Conrad et al. 1987) as the plume moves downward to the capillary fringe, where the pores are largely saturated by the aqueous phase. Once the plume reaches this region of the aquifer, NAPL that is more dense than water (DNAPL) will continue to migrate through the aquifer trapping discontinuous residual in the pores spaces unless an impermeable boundary impedes migration, causing the DNAPL to pool (Schwille 1967). NAPL less dense than water (LNAPL) will pool as a lens above the capillary fiinge after migrating through the vadose zone. As the water table fluctuates in response to local pumping or seasonal recharge and discharge, the lens of LNAPL at the capillary fiinge can become smeared over a larger region as smaller disconnected pockets of trapped residual NAPL (Hunt et a1. 1988). Regardless of whether the transport of NAPL results in the formation of a lens or a residual, NAPL components and chemicals will partition into the aqueous and gaseous phases present in the aquifer. On average, the maximum permissible level of a NAPL contaminant acceptable in water is defined by the US. Environmental Protection Agency as more than 2 orders of magnitude less than the solubility of typical NAPL contaminants (Miller et al. 1990). As a result, NAPL dissolution into the groundwater can contaminate an aquifer for decades, producing a dilute waste stream of massive volume (Hunt et al. 1988). The field application of in-situ remediation technologies for the treatment of NAPL has not achieved the high efficiency suggested by ID column experiments associated with treatability studies. This is due in part to the fact that l-D columns impose an artificial boundary that controls fluid movement between injection and recovery points. In the field however flow is free to by—pass the region contaminated with NAPL due to the resistance caused by the immiscible oleic phase within the soil pores. As a result, the efliciency of a treatment process for NAPL that relies on transport through the aqueous phase may be dramatically decreased in the 3-D in-situ environment. Compared to a lens of continuous NAPL, the resistance to aqueous flow is reduced for trapped discontinuous residual NAPL below the capillary fiinge. In this region, trapped residual NAPL occupies 10-50% of the pore space (Melrose and Brandner 1974). As a result, the resistance to the flow of the aqueous phase may still be significant enough to cause preferential flow around the contaminated region. The remediation of trapped reSidual NAPL is more arduous, as the NAPL is trapped by capillary forces stronger than the combined opposing viscous and buoyant forces. At the capillary fringe, the presence of a trapped residual gaseous phase may further accentuate the by-passing problem due to the reduced aqueous permeability in areas contaminated with trapped residual NAPL. Current remediation technologies have not identified practical methods for removing trapped residual NAPL in the saturated zone (Palmer and Fish 1992; Keely 1989). The proposed study will consider chemically enhancing the aqueous phase with surfactants to promote the dissolution of NAPL into the aqueous phase. For laminar flow conditions typical of aquifers, the dissolution of the trapped residual NAPL may be a rate- limited process resulting in less than predicted levels of NAPL contamination and clean- up efficiency (Hunt et al. 1988). 1.2 Objective and Scope of the Research The overall objective of this research is to evaluate hydraulic controls to promote the flow and residence time of surfactant enhanced water through regions contaminated with residual NAPL. The research will incorporate l-D column experiments, the development and use of a 1-D implicit transport model and the use of a 2-D numerical model with emphasis on 1) problems associated with the developing an efficient in-situ delivery and recovery design; and 2) trapped residual NAPL at the capillary fiinge. To reach these objectives, the research is conducted in six tasks, each of which define a specific objective of the research. TASK 1 Develop analytical methods for measuring NAPL concentration in a surfactant enhanced aqueous phase. 7 TASK 2 Measure the relative permeability-saturation relationship for the aqueous phase in the region where NAPL is no longer a continuum. TASK 3 Measure rate-limited kinetics of surfactant enhanced dissolution of NAPL using a flow interruption technique. TASK 4 Measure the breakthrough of a surfactant enhanced aqueous phase injected into a region of trapped residual NAPL. TASK 5 Develop a 1-D implicit transport code to model the dissolution of trapped residual NAPL in column experiments in order to view the removal of NAPL as a fiinction of time and space and evaluate pumping rates. TASK 6 Use the United States Geological Survey model for Saturated-Unsaturated Transport (U SGS SUTRA) to evaluate the efficient use of well locations as a hydraulic control in conjunction with the pumping rates optimized in Task 5 to promote the delivery/recovery of the surfactant enhanced aqueous phase into a region contaminated with trapped residual NAPL. In Task 1, an analysis method will be selected and developed after evaluating . liquid-liquid extraction methods, liquid-solid phase extraction methods and head space analysis methods. In Task 2, a trapped residual NAPL phase and/or a trapped residual air phase will be established in 1-D soil columns to simulate the region below the capillary fringe. Falling head permeability measurements will be used to compared the reduced permeability over a range of trapped residual NAPL saturation. In addition, a long term dissolution study will be conducted to measure increased aqueous phase permeability as the immiscible trapped NAPL is reduced through dissolution. In Task 3, a lumped mass transfer coefficient will be measured to predict the rate-limited dissolution of NAPL into a surfactant enhanced aqueous phase. A flow interruption technique common to measuring rate-limited processes such as thin film difliision or sorption will be adapted. In Task 4, a surfactant enhanced aqueous phase will be injected into a column with a uniform distribution of trapped residual NAPL in order to evaluated the dispersion of surfactant within a region contaminated with trapped residual NAPL. Tasks 2-4 will provide design parameters for the numerical modeling and remediation design developed in Tasks 5-6. In Task 5, the lumped mass transfer coefficient measured in Task 3 will be used to account for the dissolution of NAPL into a surfactant enhanced aqueous phase in a 1-D finite difference code which will emphasize modeling the removal of NAPL as a function of time and space. This differs from the approach of evaluating treatment techniques of predicting the rate of recovery fiom the effluent only, which essentially treats the soil column as a batch reactor. In Task 6, a region of contamination will be viewed as region of reduced aqueous permeability due to the trapped residual NAPL. Hydraulic controls will be evaluated and selected based on: 1) establishing a zone of influence which promotes flow into the contaminated region; 2) recovery of contaminant laden fluid; and 3) promoting the contact time needed to reach equilibrium or near equilibrium dissolution of NAPL into the surfactant enhanced aqueous phase, assuming that the flow paths are independent of chemical treatment. ground surface ...... ...... ..... .......... ....... ...... ......... ............ ....... ............................................ capillary fringe water table v DNAPL Figure 1.1. Schematic of an unconfined aquifer with LNAPL and DNAPL spills. Chapter 2 Background 2.1 Immiscible Fluids at the Pore Scale As most soils are hydrophobic, the surface of the soil grains maintains a continuous aqueous phase throughout the porous matrix. Within the pore space, the saturation of the aqueous phase will vary between pores saturated with the aqueous phase to soil pores where only a thin film of water may be present on the solid surface of the soil grain. A fluid immiscible with the aqueous phase, such as a gaseous air phase or a NAPL (e.g., gasoline), may also be present, but not necessarily as a continuous phase in all regions. In these hydrophilic soils, the aqueous-NAPL-gaseous (water-oil-air) phases are oriented in a soil pore as shown in Figure 2.1 (Corey 1984). The aqueous phase that preferentially wets the soil is referred to as the wetting fluid. In a two phase system, the second fluid is referred to as the nonwetting fluid. In three-phases, the phase between the wetting and nonwetting fluid is referred to as the intermediate wetting fluid. Figure 2.1 illustrates this wetting pattern in two phase systems with NAPL-gaseous phases, aqueous-gaseous phases and aqueous-NAPL phases. The order of the fluids with respect to the solid grain surface plays an important role in understanding the transport of the various phases through the porous matrix. ‘ The wetting fluid is held in the soil pores by capillary pressure. The capillary pressure, PC, is a measure of the difference in pressure across the interface of the wetting and non-wetting fluids in the soil pores, P,,w - PW. It is a function of the interfacial tension between the fluids, 0, and the radius of curvature of the interface, r (Fig. 2.2). P=P —P =— (2.1) In a NAPL spill in a hydrophilic sandy aquifer, typically, the aqueous phase is the wetting fluid and NAPL the nonwetting fluid. In aqueous-gaseous phase systems, the bubbling point pressure, or air entry pressure, has been defined as the pressure needed to force the gaseous phase into a capillary tube while draining the water out. A similar definition applies to NAPL displacing the aqueous phase. The NAPL entry pressure is the pressure needed to displace the aqueous phase held in the soil pores by the capillary pressure. Since capillary pressure is inversely proportional to the radius of curvature, a higher NAPL entry pressure is needed to displace the aqueous phase held in the smaller pores and pore throats. As a result, NAPL penetrating a region where the aqueous phase saturates the pores will displace the aqueous phase from the larger pores first. However, when the aqueous phase is reintroduced into the pores, the stronger capillary forces in the smaller pores and pore throats will pull the aqueous phase into these pores spaces first. 2.2 NAPL Entrapment as a Discontinuous Residual Phase The petroleum industry has studied the mechanisms of residual oil entrapment and recovery for secondary and tertiary recovery. A brief overview of this work is presented in this section. The distribution and trapping of trapped residual NAPL, or ganglia, is influenced by the geometry of the pore spaces, fluid and soil interfacial properties, the interfacial tension between the fluids, pressure gradients and gravitational forces (Morrow and Songkran 1981). These factors can be evaluated in two dimensionless numbers which incorporate viscous (F v), buoyant or gravity forces (Fg) and interfacial tension ([F'I') forces (Ft). Fg = mg = Apl3g (2-2) Fv = 1A = p[$)A Ep(;)lz =pvl (2.3) Ft = 01 (2.4) where m is mass, g the gravitational constant, Ap the density difference, I stress, A cross sectional area, it viscosity, v velocity, 1 a characteristic length, and o interfacial tension. The capillary number, No, reflects the ratio of viscous forces to capillary or surface tension forces , whereas the bond number is the ratio of buoyant or gravity forces to capillary forces (Morrow and Songkran 1981; Larson et al. 1981). Nc=L‘_‘-_-kw_Ae (2.5) a la 2 NIL—Jill}: (2.6) a where kw is the permeability of the wetting phase and R the radius of a grain of soil. Morrow and Songkran (1981) found that for Nb less than 0.00667, mobilization and entrappment are more strongly influenced by changes in the ratio of the capillary to viscous forces as opposed to the relationship between the buoyancy and capillary forces (Fig. 2.3). Table 2.1 reviews past research in trapped residual NAPL which indicates that a range of trapped residual NAPL saturation (Sm) can exists in sands. A similar review is presented in Mercer and Cohen (1990). 2.3 Hydraulic Conductivity and Permeability Hydraulic conductivity, K, is a measure of the resistance to fluid flow through porous media. It is a function of both the fluid and soil properties: K: has (2.7) p where It is the permeability of the soil, p is the density of the fluid, u is the viscosity of the fluid and g is acceleration due to gravity. In a two- or three-phase system, permeability is also considered to be a fiinction of the fluid phase saturations (Fig. 2.4). In the absence of the nonwetting fluid, the relative permeability of the wetting fluid is 1. Once the nonwetting fluid is introduced, the permeability of the wetting fluid decreases as the saturation of nonwetting fluid in the pores increases. Conversely, if the wetting fluid is reintroduced into the pore space the permeability of the wetting fluid will increase as the saturation of the nonwetting fluid decreases. At low hydraulic gradients common to ground water systems, water reintroduced into the soil pores cannot completely remove the non-wetting fluid (Wilson et al. 1990). Instead, the non-wetting fluid becomes immobile, discontinuous and trapped by capillary pressures stronger than the combined viscous and buoyant forces. Within these pores, the maximum saturation of water (Sm) is limited by the trapped residual saturation of the non-wetting fluid, which in turn limits the permeability of water. As discussed previously, the aqueous phase is a continuous fluid within the porous matrix. The residual saturation of the aqueous phase is defined as the irreducible aqueous phase where the aqueous phase is at a minimum (Sm). The trapped residual NAPL phase is defined as Sm in Figure 2.4. If permeability in a contaminated region is reduced due to the oil present in the soil pore, streamlines will deflect at least partially around the region, resulting in a smaller flux of water through the contaminated region. Wheatcraft and Winterberg (1985) showed that the fiaction of flow that would pass through a cylinder of reduced permeability relative to the amount that would pass through the cylinder if the entire region was homogeneous in a uniform flow field can be calculated from: F“ = 2k,/(1+ k,) (2.8) where k, is the permeability of the cylinder relative to the permeability of the surrounding medium (Fig. 2.5). Consider a circular region where the permeability is reduced (i.e., regions where k, = 0.6, 0.3, 0.1). A comparison of the fraction of flow, Fm, through these circular regions of reduced permeability with flow passing through a comparable cross-section where k, = 1 resulted in values of Fa, equal to 0.75, 0.46, and 0.18 for the 10 respective three regions of reduced permeability. These preliminary results support the need to evaluate the reduced permeability when designing an in-sr’lu ground water technology targeting immiscible contaminants. The use of hydraulic controls to promote flow paths through regions of reduced conductivity in the field are not well understood. Analytical and numerical solutions to groundwater flow problems have traditionally focused on the flow paths created by hydraulic controls in homogeneous aquifers (Bear 1979; White 1979). These studies can provide the basis for evaluating the initial placement of injection/recovery wells and pumping rates. The results will be different, however, once the heterogeneous region resulting fi'om the reduced permeability of pores with trapped residual NAPL is included. 2.4 Mobilization of Trapped Residual NAPL Past research in both petroleum engineering and environmental remediation engineering has focused on removing trapped residual NAPL through mobilization. With mobilization, the trapping of residual NAPL is controlled by capillary forces stronger than the combined viscous and buoyant forces present. Past remediation research has considered reducing No by either hydraulically increasing the gradient (Wilson and Conrad 1984) or chemically enhancing the groundwater to reduce the interfacial tension (Texas Research Institute 1979; Abdul et al. 1992; Ellis et al. 1984; Nash and Traver 1984). Wilson and Conrad (1984) considered increasing the hydraulic gradient in both horizontal and vertical sweeps to mobilize residual hydrocarbons in the saturated zone. They concluded that for k > 100 cm2 (coarse sand and fine gravel), residual blobs could be mobilized in both horizontal and vertical sweeps. In addition , for k > 1 cm2 (sandy silt or fine sand), residual blobs could also be mobilized in a vertical sweep, but not in horizontal sweeps. For k < 0.1 cm2 (glacial till, fine silt, clay), sufficiently high gradients cannot be achieved, vertically or horizontally, to mobilize residual oil in the saturated 11 region. As an applied technology, this method is limited by the practical constraints of establishing the higher hydraulic gradients in the field (Wilson et. al 1990). The capillary number can also be increased by lowering the IFT between the NAPL and water sufficiently to allow the capillary force to overcome the combined viscous and buoyant forces so that oil can be released from the pore space. Petroleum engineers have measured the reduction in the residual trapped NAPL (Sn/8*m) as a function of the capillary number (Fig. 2.6) . In studies of sandstone and glass bead packs, residual oil was completely removed at Nc > 10'2 (Chatzis and Morrow 1981,1984; Morrow and Chatzis 1982; Morrow et al. 1988). The critical Nc is defined as the point where mobilization of the residual non-wetting fluid begins. Wilson et al. (1990) measured the critical No in Sevilleta sand at Nc = 104, which falls between the critical Nc for sandstone and glass beads (10'5 and 103, respectively). Surfactant enhancement of the aqueous phase can alter the interfacial tension by 4 orders of magnitude (Fountain et al. 1991), which may reduce the Ne sufficiently to cause mobilization. By enhancing the aqueous phase with surfactants to lower the interfacial tension, the residual can be ' mobilized. Ng et al. (1978) showed that mobilized residual oil will migrate into adjacent pores and coalesce with an existing ganglia. As released residual continues to coalesce in this fashion, the permeability of water will begin to decrease as the oil saturation increases. Eventually, the decreased permeability will significantly reduce the flux of surfactant into the pores (Texas Research Institute, 1979). This loss in efficiency results in an increased cost for the technology. In the case of residual DNAPL trapped within and below the capillary fiinge, the released contaminant threatens to migrate deeper into uncontaminated regions of the aquifer. The problems associated with IFT surfactants and delivery are suggested in a well documented pilot scale study by the U. S. Environmental Protection Agency at the Volk Air National Guard Base, Camp Douglas, Wisconsin. This in-sr'tu remediation targeted the use of surfactants to remove NAPL in the vadose zone. Prior column studies 12 suggested removal efficiencies as high as 98% after flushing with 12 pore volumes of surfactant (Nash and Traver 1984). However, the in-situ pilot scale was not measurably effective in removing 'the contamination after 14 pore volumes. The final report could not cite conclusive reasons for the pilot scale failure. It does cite a plausible explanation, namely that surfactant may have flowed in preferential pathways created in regions containing smaller fractions of the more highly contaminated fine soil (Nash and Traver, 1985). In addition, if the soil contained a high level of fines, the surfactant may have caused a dispersion of colloidal size particle which could lead to clogging of the soil pores and a reduction in flow (Abdul et al. 1990). However, an alternative explanation can be found if one views the reduced aqueous flow within pore spaces resulting from the coalescing of released residual NAPL. The increased saturation of NAPL collecting in the pores spaces will create a blockage, resulting in reduced permeability. Unrestricted by a boundary (i.e. column walls) the flow is free to flow through areas of higher conductivity around the contaminated regions. Petroleum engineers have combined polymers with surfactants to aid in mobility control of the released NAPL by increasing viscosity while mobilizing residual oil (Sale and Pitts 1989; Smith 1966). The significance of increased viscosity can be explained by examining the mobility ratio, MR. _ mobility of displacing fluid _ km ,u" (2 9) mobility of displaced fluid ‘ km p, ' where Iran, is the effective permeability of the aqueous phase at the residual NAPL saturation, [rum is the effective permeability of the NAPL at residual aqueous phase saturation, ua is the viscosity of the aqueous phase and w: the viscosity of the NAPL. As the change in interfacial tension mobilizes residual oil, the decreased saturation of the residual oil will result in an increase in the permeability of water. As a result, the mobility ratio will increase. This increase may result in fingering of the displacing fluid 13 past the displaced fluid, minimizing the contact of the surfactant with the contaminated region. The addition of polymers to increase the viscosity of the aqueous phase is intended to counterbalance the increase in aqueous permeability. A surfactant-polymer pilot scale study was conducted to remove residual DNAPL at a former wood testing site in Wyoming with reasonable success (Sale et al. 1989). In this system, an impermeable lower boundary provided a barrier to released DNAPL migrating into uncontaminated regions of the aquifer. 2.5 Surfactants Surfactants, or surface active agents, have a characteristic amphipathic molecular structure consisting of a lyophobic structural group that has very little attraction for the solvent together with a lyophilic structural group which has a strong attraction for the solvent (Rosen 1989). In water soluble surfactants intended to enhance the dissolution of NAPL, the solvent is water and the solute is NAPL. In aqueous system, the lyophobic and lyophilic structural groups are ofien referred to as hydrophobic and hydrophilic. At low concentrations in water, surfactants begin to orient with the hydrophilic ends toward and the hydrophobic end repelled away from the aqueous phase. Eventually, the critical micelle concentration (CMC) will be reached. At this concentration, colloidal sized clusters called micelles begin to form which can solubilize nonaqueous fluids into the aqueous phase (Fig. 2.7) At the CMC, breaks in the trend of other measurable physical properties including surface tension, detergency, osmotic pressure, equivalent conductivity and interfacial tension also occur (Fig. 2.8). The micelles capture the NAPL by surrounding it with the hydrophobic ends. Once trapped in the micelle, the NAPL moves in the same phase as the water. As a result, surfactants make it possible to solubilize normally insoluble substances. Solubilization can be distinguished fi'om emulsification, which is the dispersion of one phase into another, with each phase remaining distinct. As the amount of NAPL is increased in the interior hydrophobic core, 14 a micelle will become more and more asymmetric, eventually becoming lamellar in shape. In theory, this process can be reversed by adding water to decrease the concentration of surfactant. Interfacial tension is a measure of the minimum amount of work required to create an interface. At the interface, molecules have a higher potential energy than interior molecules due to the fact that molecules interact more strongly with molecules in the interior. Work is required to bring the molecules to the surface. When water is enhanced with surfactant, the hydrophobic group will increase the fi'ee energy of the system. This means that less work is required to bring a surfactant molecule to the surface than a water molecule. As a result, surfactants concentrate at the interface, with the hydrophilic tails oriented inward and the hydrophobic tails at the interface (Rosen 1989). The use of surfactants which increase the solubility of NAPL into the aqueous phase addresses some of the problems associated with IFT surfactants, yet there is still a threat of spreading the contamination to new regions if the flow carrying contaminant bearing micelles is not recovered. Consequently, the need to establish hydraulic control is essential for recovery as well as delivery of the surfactant. In addition, recovering the surfactant for recycling can lower the costs of in-situ surfactant flushing (Clarke et al. 1992). 2.6 Kinetics of Surfactant Enhanced Dissolution Ifthe flow rates during remediation are too rapid to allow the surfactant enhanced water sufficient contact time with residual NAPL for the surfactant to achieve the maximum solubility of NAPL, the technology will produce large volumes of mildly contaminated water. As a result, the expense involved with both the surfactant and the treatment of the waste water may render the technology prohibitive from an economical viewpoint. Intermittent (pulsed) pumping has been suggested to address the inefficiency resulting from non-equilibrium (Keely 1989). In this pump and treat method, the cycling 15 of injection/extraction well pumping schedules is based on promoting the residence time needed for water to come into localized equilibrium with trapped residual NAPL. Preliminary studies were conducted by Pennell et a1. (1992) to measure the solubility of dodecane in surfactant as a function of pore water velocity and the duration of flow interruptions. They concluded that pulsed (intermittent) pumping is more efficient than continual pumping. In contrast, Ang and Abdul (1991) conducted two 1-D column experiments comparing intermittent vs. continuous pumping which showed no significant difl‘erence in surfactant removal efficiency for removing residual automatic transmission fluid from sandy soil. A numerical simulation study by Borden and Kao (1992) of intermittent pumping concluded that the greater amount of hydrocarbon recovered per volume water may increase the time required to meet a specific remediation standard. These different conclusion emphasize the need to conduct site specific studies. 2.7 Surfactant Transport of Solubilized NAPL When a continuous tracer is introduced into the aqueous phase of the porous media, it will be advected by the groundwater flow. In addition, it will also spread out laterally and longitudinally, occupying an ever increasing portion of the flow domain. This spreading phenomenon is called hydrodynamic dispersion (dispersion, miscible displacement) in groundwater (Bear 1979). The one-dimensional form of the advection- dispersion equation for a non reactive dissolved constituent is 2 at 3:: fix for saturated, homogeneous, isotropic materials under steady-state, uniform flow (Freeze and Cherry 1979). In this equation, C is the concentration of the solute in the aqueous phase, D is the coefiicient of hydrodynamic dispersion, v is the average linear velocity, 1 is time and x is the spatial coordinate. 16 This equation may be written in the non-dimensional form (Brusseau and Rao 1989) aC'_ié’2C’_§C° at. Pe 6X2 é’X (2.11) by introducing the following dimensionless parameters: (3.ng Pe=% ° (2.12) . vi t = I X =% In Eqn. 6.11-12, C * is the dimensionless concentration, C0 equilibrium concentration, Pe the Péclet number, L the length of the column, t* dimensionless time (pore volume), and X dimensionless distance. The slope of the breakthrough curve, which is a measure of the magnitude of the dispersion, is a fiinction of Fe. The coefficient of hydrodynamic dispersion may be determined fi'om the slope of the front part of the breakthrough curve. It can be expressed in terms of two components: D: m7+D' (2.13) where dispersivity, a, is a characteristic property of the porous media, and the coefficient of molecular difi‘usion, D', is a characteristic of the solute . At high velocity, dispersion is dominated by mechanical mixing relative to the effects of molecular diffusion. At low velocity, dispersion due to molecular diffusion dominates (Freeze and Cherry 1979). When an aqueous surfactant is continuously injected into a region of the groundwater system to enhance the aqueous solubility of an immiscible residual NAPL, it will exhibit the same behavior as that of a tracer, with dispersion influenced by the properties of the fluids and the porous media. A breakthrough curve measuring the concentration of NAPL in the surfactant will provide a measure of the zone of influence 17 created by the transport of NAPL solubilized into the surfactant enhanced aqueous phase. However, the chemical processes of surfactant solubilization in the porous matrix are also influenced by surfactant sorption to the soil, which may also exhibit nonequilibrium. Theoretically, surfactant sorption without nonequilibrium will shift the breakthrough curve to the left. In contrast, mass transfer limitations due to dead-end pore spaces and increases in local flow velocities as a result of trapped residual NAPL restricting flow paths can shift the breakthrough curve to the right. As a result, a 1-D column study to measure the breakthrough curve of surfactant injected into soil with trapped residual NAPL integrates the complexity of different chemical and flow processes of dissolution, sorption and variability in ganglia size and shape. Figure 2.1. Schematic of pore space characteristics. 18 Figure 2.2 Pressure difference at the interface of immiscible fluids in an idealized pore throat or pore body. 16 a— 14 —~ :i 12 —a O 2, 10 ~~ :> 8 .- a a 4 _. 5° 2 «L- o i i i i 10:7 10’6 10'5 10’4 10'3 CAPILLARY NUMBER Figure 2.3. Relative effect of the capillary number as a function of trapped residual saturation at Bond numbers less than 0.00667 (adapted from Morrow and Songkran 1981). l9 IRREDUCIBLE ——’ WETI‘ING SATURATION TRAPPED RESIDUAL N APL k, SATURATION _’ ‘— nonwettin g phase 0 —> S (wetting) 1 1 S (nonwetting) <— 0 Figure 2.4. Relative permeability as a function of phase saturation. 1 r 0.9 .. 0.8 a” 0.7 .. 0.6 ‘- 3 0.5 ‘r ta? 0.4 .. 0.3 ‘- 0.2 ‘- 0.1 ‘- 0 i + . . . 0 0.2 0.4 0.6 0.8 1 kr Figure 2.5. Flow passing through a permeable cylinder in a uniform flow field relative to the flow passing through the clinder when k, = l (Wheatcraft and Winterberg 1985). 20 0.9 r“ 0.8 " 0.7 y- 0.8 ‘* 0.5 ‘1“ an/STI-n 0.4 «r 0.2 «r- o.1 .. 0 i i i v 10‘6 105 Hr4 I0’3 10'2 CAPILLARY NUMBER Figure 2.6. Relative correlation of the mobilization of residual oil and the capillary number for uniform glass beads (adapted from Morrow et al. 1988). HYDROPHOBIC . 15:, , 1.3:: 523:2. ND HYDROPHILIC 535:3?" END IMMISCIBLE CONTAMINANT Figure 2.7. Schematic of a surfactant micelle capturing an idealized NAPL ganglia. 21 Critical Concentration Equlvalent conductivity Interfacial CONCENTRATION (2.) Figure 2.8. Relative changes in physical properties in the neighborhood of the critical micelle concentration (adapted from Preston 1948). 22 SOIL s,” (%) REFERENCE OTTAWA 12 POWER ET AL. 1992 SEVILLETA 27.1 WILSON ET AL. 1990 TRAVERSE CITY SOIL 15.8-19.3 WILSON ET AL. 1990 LLANO SOIL 13.9-18.5 WILSON ET AL. 1990 GLASS BEADS 14.25 CHATZIS ET AL. 1983 SANDSTONE 30-40 MELROSE AND BRANDER 1974 SEVILLETA 23-34 CONRAD ET AL. 1987 SANDSTONE 11-30 ' CHATZIS ET AL. 1988 SANDSTONE 27-43 CHATZIS AND MORROW 1984 OTTAWA SAND 15.9-20.4 PENNELL ET AL. 1993 WAGNER 18 SAND 8.4 POWERS ET AL. 1992 WAGNER 50 SAND 12.3 POWERS ET AL. 1992 OTTAWA SAND 12 POWERS ET AL. 1992 WAGNER MIX 16.5-18.5 POWERS ET AL. 1992 SEVILLETA SAND 22.5 MACE AND WILSON 1992 SAND/SILT/CLAY 16.9-30.3 MACE AND WILSON 1992 AQUIFER SAND 34-41 ANG AND ABDUL 1991 GLASS BEADS 121-14.06 MORROW AND SONGKRAN 1979 Table 2.1. Overview of past research in NAPL entrapment and mobilization. Chapter 3 Materials and Methods This chapter presents an overview of the materials and methods used in the experiments presented in Chapters IV and V. A majority of the experimental work is conducted in 1-D glass columns using white Ottawa sand, dodecane and a 5% solution of a nonionic surfactant, Witconol NP-150, although some batch experiments used in the early stages of investigation are also described. Methods are outlined for packing and saturating the soil column, establishing a trapped residual NAPL, measuring permeability, determining the equilibrium solubility of NAPL in surfactant, measuring the kinetics of surfactant enhanced dissolution and dye sorption measurements. A section addressing error analysis is also presented. 3 .1 Apparatus A borosilicate glass column designed to minimize sorption losses and to maintain a hydrophilic surface (Zalidis et al. 1991) was modified for use in this research (Fig. 3.1). The column was altered for saturated soil experiments by removing the porous pressure plate fiom the bottom of the column. In addition, the experiments conducted in saturated soil do not require a venting port in the top cap. The column was designed for easy assembly and disassembly. The length of the threaded rods can be changed to accommodate different column lengths. In addition, Viton® o-rings, stainless steel screens and Teflon® caps were used to maintain hydrophilic surfaces which minimize sorption losses. 23 24 3.2 Preparation of Soil Column Prior to packing the 1-D column, the individual components are washed and oven dried. The total weight of all components was measured for later determination of soil and fluid mass (Fisher Scientific Top Loading Balance Model # XT1200DR). The bulk density, Pb, was determined from the dry weight of the assembled column. "Mafia V 6' p1» (3-1) where Md is the mass of the column with dry soil, MC is the mass of the column, and V0 is the volume in the column. The soil packed column was subjected to a 700 mm Hg vacuum (Vacu/Trol Lab Vac. Regulator with pump, Spectrum Medical Industries, Inc., Patent Pending) for 30 minutes to remove the gaseous phase. The column was then slowly saturated fi'om the bottom with deaired deionized water. The column was weighed to determine the saturated weight of the column to estimate the pore volume (PV) and porosity (n) of the soil. PV= Mi'Md —V (3.2) p caps n = g (3.3) where M, is the mass of the water saturated soil column and Vcaps the volume in the caps. . 3.3 Establishing a Trapped Residual Irnnriscible Phase The following procedure outlines the method for establishing a residual NAPL in the soil column. Dodecane was flushed through the top of the water saturated column to assure a stable displacement of the aqueous phase (Kueper and Frind 1988) under approximately 1 psi of pressure. Once the NAPL reached the bottom of the column (as 25 evident through a liquid color change observed in the effluent), the flow of water out of the bottom of the column was interrupted, while the pressure remained on the oil. After 1/2 hour, the aqueous flow was reintroduced through the bottom of the column using a syringe pump (Harvard Apparatus Syringe Infirsion Pump 22, Model # 55-2219) equipped with 140 cc Monoject® syringes. The effluent was monitored for free phase NAPL. Trapped residual NAPL was observed in the soil pores near the column wall in regions where the flushing water removed continuous NAPL. The column was flushed with a minimum of 5 additional pore volumes of water after free NAPL was no longer observed in the effluent to assure that all mobile continuous NAPL was removed, simulating naturally occurring aquifer conditions which would trap NAPL as a residual in the saturated region of an aquifer. When the column was disassembled, the residual trapped NAPL was observed to be relatively uniformly distributed throughout the soil. Flux rates of the infiltrating water were varied but maintained within the range of velocities to assure laminar flow in the soil columns. In porous media, the upper limit of Darcy flow to assure laminar flow is achieved by maintaining the Reynolds number (Re) between 1-10, although Re = 100 is often mentioned as an upper limit (Bear 1979; Freeze and Cherry 1979). pvd ,u Re = (3.4) where p is the density of the fluid, v the velocity, d a characteristic length (e. g., diameter of the soil grain), and u the viscosity of the fluid. The saturation of trapped residual NAPL in the porous media, Sm, was estimated to be (Wilson et al. 1990) S... = M__M_ (3.5) Ap PV 26 where Mm is the mass of the soil column after a trapped residual NAPL saturation is established. To simulate conditions in the upper region of the capillary fiinge, a trapped residual gaseous phase was established by flooding a water saturated column with the gaseous phase under 5 psi of pressure, followed by a minimum of 5 pore volumes of water. An additional trapped residual NAPL was established in these columns to simulate conditions in the upper region of the capillary fiinge by following the previously outlined procedure for trapping residual NAPL in water saturated pores. 3.4. Hydraulic Conductivity Measurements Hydraulic conductivity, K, was measured using the falling head method (Klute 1986) for initial experiments where K =(%,)1n(1%2) (3.6) where a is the cross sectional area of the standpipe, A the cross sectional area of the soil sample, 1 is time, L is the sample length and H1 and H 2 measurements of the initial and final hydraulic head (Fig. 3.2). For the experiment where the relative permeability of the aqueous phase was measured during continuous surfactant pumping, conductivity was measured by the pressure difference across the column using a water manometer. 19$ AAH (3.7) where Q is the flux rate, L the length of the column and AH the hydraulic head difference across the column (Fig. 3.3). Initial experiments were conducted to measure and account for the head loss across the apparatus without soil. 27 3.5 Equilibrium Solubility of NAPL in Surfactant Batch experiments where used to determine the equilibrium solubility of dodecane over a range of surfactant concentrations in an aqueous solution. Ten [.11 of dodecane were injected into 10 ml of surfactant in glass vials with butyl rubber/PTFE septa and aluminum caps. The vials were placed on a shaker apparatus for 24 hours after which the fluid contents was allowed to stratify for 24 hours in the vials with the septa side facing down. Samples were taken from the bottom of the vials and analyzed for dodecane concentration. 3.6 Investigation of the Kinetics of Surfactant Enhanced Dissolution of Trapped Residual NAPL To investigate nonequilibrium effects of surfactant enhanced dissolution, a residual NAPL phase was initially established in a saturated soil column. A 5% surfactant solution was pumped into the column at a flux of 10 ml/min. This faster perculation rate maintained a minimal dodecane concentration at the initiation of the pulsed pumping while assuring 1 < Re < 10. After flushing the column with 2 pore volumes of surfactant, the pumping was discontinued. Surfactant was allowed to remain in static contact with the residual NAPL for intervals ranging from 1-72 hours. At the end of the specified interval, pumping was resumed, collecting 5 ml samples at the effluent end after 0.25 pore volumes. After pumping 2 pore volumes of fresh surfactant into the column, the pumping was again discontinued for a specified period of time. Experiments were also conducted to compare the solubility of trapped residual dodecane into the surfactant enhanced aqueous phase when the contact time was achieved from continuous pumping, as opposed to static contact, through, a contaminated region. In these experiments, the surfactant contact was controlled by varying the pumping rate between 0.24-1 ml/min, resulting in residence times from 2-10 hours. 28 3.7 Dye Sorption Measurements To observe the immiscible fluid movement and entrapment in the porous media, the NAPL was dyed with an oil soluble dye, Oil Red 0 biological stain obtained from the Aldrich Chemical Company (Milwaukee, Wisconsin). In these experiments, the mass of soil that was placed glass vials with a fixed volume of dyed oil was increased. The vials were well mixed on a mechanical mixer for 24 hours. The concentration of dye in the fluid was then determined by ultraviolet (UV) analysis using a Hewlett Packard 8452A diode array spectrophotometer. 3.8 Error Analysis Uncertainty was estimated using a finite divided difference approximation of the Taylor series where the overall uncertainty interval, 6R, is calculated as 5R: {glggdsfr n V: {Elm + 6x.) — R ........ 5% ,4 1.4 __ A 2.50% A ‘— ‘ o i 3 1.2 1.25%: D E 1 - D 0.60% ,.4' D :5 0.8 —~ --------- ., ------ 0.30% I E 4 U A < 0.6 -- " ‘ 04 D A A __,4 A 02 — -- a ‘ A ...................... 0 A IIIIIIIIIII é ‘‘‘‘‘‘‘‘‘‘‘‘‘‘‘‘‘‘‘‘‘‘‘‘‘‘‘‘‘‘ O ............................................ 0 ............... 9f . . { ' e . 0 1 2 3 4 5 6 7 8 9 10 Cone. of Dodecane (ppm) Figure 4.1. GC response to dodecane concentration at varying surfactant concentrations illustrating the effects of surfactant concentration on partitioning of dodecane. —D— DODFCANE W/O SALT —‘°_ WDFCANE W/SALT AREA/le6(uV‘see) c88888888 A . . . _ _ 05 r 1.5 2 25 3 3.5 4 45 5 Corie. d'WIfcaId Nit-150w.) O Figure 4.2. GC measurement of 4 ppm dodecane in varying surfactant concentrations with salt. 53 Cone. of Witconol DIP-150 (%) la) -- 160 *- —C}—- 3‘ 140 “ DODBCANE 5 1m .. "" A WANE 5 1(1) .. 3 30 .. 2 g m 4% < 40 .. 20 .. 0 . . . . r . . t fl: 0 0.5 l 1.5 2 2.5 3 3.5 4 4.5 Ur Figure 4.3. Four ppm undecane at varying surfactant concentrations. 12 160 -- I” «h —0— 95/30 / _.x__ m -- ”/60 R=o.992 Y=14.14X+8.6 ’3‘ —0— 80/30 8 ‘00 ‘" R=0.998 Y=15.00X+2.2 V ‘8 80 ‘- - R=0.998 Y=6..17X+19 a 60 . // // ‘0 T // R=0.995 Y=6.0.8X+17 m .. 0 JF// , 4 a o 2 4 6 s 10 Cone. of Dodecane (ppm) Figure 4.4. The influence of thermostat temperature and equilibrium time (temp/time) on calibration curves. 54 2500 l 2500 .. 2000 l 0 2000 0 3 A (‘3 A E g 1500 4 E 5 1500 4 J v _’ V g ‘i‘ g ‘5 .1 5 1000 . 0 O 5 1000 -. 0 00) “J a) u’ 3 § 500 " 0 3 § 5‘” «1» O 0 O 0 -———<)—0—<>—A ne- 9 O 9 a O @O t c . . . 0.001 0.01 0.1 1 10 o 1 2 3 4 5 as SURFACTANT (WITCONOL NIP-150) ‘56 SURFACTANT (WITCONOL NP-150) Figure 4.5. Equilibrium solubility of dodecane in varying concentrations of Witconol NP-150. 8 8 8 N C Surface Tension (dynes/cm) 8 ‘5 WWW—LAM O - 0.0001 0.001 0.01 0.1 1 10 Cone. of Witconol PIP-150 (%) Figure 4.6. Critical micellar concentration of Witconol NP-150 determined from surface tension (Witco 1991). 55 1.0- 08- 06- on a 04- 6 Raw Data -——m——— :: '1 02, k I 0.387 hr —1t,=0.161hr'l 00- , 1 1 r I T ' T ' I o 5 10 15 20 25 Residence Time (hr.) Figure 4.7. Flow interruption study. 16- 4 141-- 12'- Relmive Error (%) 6 4 A A A 00 02 O4 08 .08 1.0 Figure 4.8. Error associated with enhanced solubility measurement in flow interruption study. 56 1 l . O O 0.8 «» ° 4’ 4 .1 0.6 ’4. 4 ’ 4., .° 0 ° , ° 2 . .. O . O U 0.4 ° 0 N 0.2 . sTOP CONTINUOUS PUMPING 0 ¢ 4 4 t t 0 20 40 60 80 100 120 t* Figure 4.9. Continuous pumping of Witconol NP-150 followed by a water flush and subsequent pulsed pumping. 1.00 .. 1.00 l 0.80 .. 0.80 t» g 4 4 4 ° 0 44 , . 4 4 4 9 O . 4 ° a 060 .. 4" .. 0.60 .. ” O 4 U D 040< ° O 040 °. ' . Srn=14.8'/t ' Sm =13.1°/. 0.20 ’ 0.20 t . 4 .4 0m m‘“ “““‘ "52“.: 4 4 4 0m --—4+.-o—++M—4———4———4 0000 0.500 1.000 1.500 2000 2500 0.000 0.500 1.000 1.500 2.000 t. t O 100 1.00 0.80 1» 030 .. g 400. 0 . 4 n 0.60 .. ”4.. ° ° 0 ° a 0.60 -- 4’ ° 0 4 Q 4 U 4 0.40 <- 0 040 .. 020- 5m: 160% 020 .0 Sm -18.0% 0 0 0m a———O-O-O+M——4——+———4——t 0m «t—W—OW—WM‘Q—fi—t—fl 0.000 0.500 1.000 1.500 2000 2500 0.000 0.200 0.400 0.600 0.800 1.000 1.200 1.400 t. t. Figure 4.10. Breakthrough curves for 5% Witconol NP-150 injected into regions of trapped residual dodecane. 57 12 7' 0 10 it 0 13.10% M O 8 -t>— g ‘ 14.80% E 6 A 16.00% a 4 0 18.00% 0 O 2 a! a 0A O 0 iii 9 4 at tam—WW 0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 C/Cs Figure 4.11. Error associated with break through curves. LN 1' 0.” 1r °Sln=11196 ‘ o 88 0° RfiAfiédAa‘ ‘ A ‘ ‘ ‘ A 0.50 .. A Srn=14.8% geinA a A A; ‘ 8 ASrn=16.0% A .0 0.404 ostn=raosi A ° ‘ ‘ O 0.1)» 4 000A 0 am-i—MWQA‘; 1 $ % 0.” 0.51!) HID 1.5m . 201) 2.5“) t. Figure 4.12. Compilation of breakthrough curves. 58 Sample temperature 95° Needle temperature 120° Transfer temperature 120° G.C. cycle time 10 minutes Thermostat time 30 minutes Pressurized time 2 minutes Inject time 0.15 minutes Withdraw time 0.2 minutes Oven temperature 125 ° C Carrier gas (Helium) 200 ml/min Table.4.1. G.C. Settings. Exp. Sm Relative Relative pb Relative Error (%) Error (%) Error (%) 1 0.148 2.533 0.376 0.484 1.766 0.058 2 0.160 2.427 0.401 0.479 1.803 0.058 3 0.131 2.668 0.369 0.486 1.854 0.058 4 0.180 2.381 0.383 0.483 1.840 0.058 Table 4.2. Experimental set-up for breakthrough curves. Chapter 5 Aqueous Permeability Prior to and During Surfactant Enhanced Dissolution of Trapped Residual NAPL 5 .1 Introduction Once introduced into the groundwater environment, a spill of nonaqueous phase liquid (NAPL) will migrate through the vadose zone of the soil. If the volume is sufficiently large, the spill will reach the capillary fiinge where isolated ganglia of NAPL can become trapped as a discontinuous residual phase. Once discontinuous, the NAPL becomes a continual source of groundwater contamination that is not easily addressed by conventional pump-and-treat remediation technology (Hall, 1989). Removal is only possible by the slow dissolution of the NAPL into the aqueous phase, since the NAPL is essentially immobilized by capillary forces stronger than the combined viscous and buoyancy forces. On average, the maximum permissible level of a NAPL contaminant acceptable in water is defined by the US. Environmental Protection Agency as more than 2 orders of magnitude less than the solubility of typical NAPL contaminants (Miller et al. 1990). As a result, NAPL dissolution into the groundwater can contaminate an aquifer for decades, producing a dilute waste stream of massive volume (Hunt et al. 1988). Aqueous surfactants can be injected into the groundwater to enhance the solubilization of NAPL into colloidal size clusters known as micelles. Once trapped in the micelle, the NAPL moves in the same phase as the aqueous phase (Rosen 1989). The added expense of surfactants to pump-and-treat methods accentuates the need for efficient delivery of the treatment into contaminated regions. 59 The limited number of field applications to date of in-situ remediation technologies for the treatment of non-aqueous phase liquids (N APL) have not achieved the high efficiency suggested by 1-D column experiments (Ellis et al. 1984; Nash and Traver 1984; Nash 1985). This is due in part to the fact that 1-D columns impose an artificial boundary which controls fluid movement between injection and recovery points. However, in the field flow is free to by-pass the low conductivity NAPL contaminated region due to the lack of confinement of flow boundaries that coincide with the boundaries of the contaminated region. Since many in-situ technologies rely on transport through the aqueous phase, the reduced aqueous conductivity in. the contaminated region may result in some fraction of the treatment by-passing the area targeted for remediation. This resistance can be decreased if the NAPL saturation is reduced through pumping, NAPL migration or, as in the case of LNAPL, spread over a larger range due to watertable fluctuations (Hunt et al. 1988). The remaining residual saturation is far more difficult to remove, trapped by capillary forces stronger than the combined opposing viscous and buoyant forces. In the saturated region, residual NAPL occupies between 10-50% of the pore space (Wilson and Conrad 1984). Hence, the pore blockage resisting flow may still be significant. The problems caused by blockage may be accentuated in the capillary fiinge, where a trapped residual gaseous phase is also trapped within the soil pores due to imbibition and drainage in the capillary fiinge from infiltration and water table fluctuations (Corey 1984). Relative permeability-saturation curves are used to predict the flow of two immiscible fluids within a porous media. Within the matrix, the wetting phase fluid is physiwa limited fi'om reaching firll saturation or its maximum relative permeability within the pores if the non-wetting phase is trapped and discontinuous (Fig. 2.4). Petroleum engineers want to mobilize trapped residual oil, which is the nonwetting fluid with respect to the aqueous phase, which remains after a normal waterflood in petroleum reservoirs. As a result, past petroleum engineering research has focused measuring the 61 relative permeability of the aqueous phase at Sa 2 1 - Sm. in sandstone cores (Morrow et al. 1985; Gilliland and Conley 1975; Amaefiile and Handy 1981) and glass beads (Morrow and Songkran 1981). In these experiments, the saturation of the NAPL was reduced by lowering the interfacial tension between the aqueous phase and the NAPL or by increasing the pressure gradient. It has been shown. that the pressure gradients required to mobilize trapped residual NAPL in aquifers is unrealistic (Wilson and Conrad 1984). Mobilizing trapped residual oil may cause the oil to migrate into previously uncontaminated regions of the aquifer, a problem accentuated in the remediation of DNAPL. However, experiments measuring the aqueous phase permeability in regions over a range of trapped residual NAPL saturations may provide design values germane to developing remediation strategies. However, the effect of the interfacial tension on the relative permeability curves of the aqueous phase has been evaluated with conflicting results. Gilliland and Conley (1975) extend the curve for the relative permeability of the aqueous phase from Sa 2 1 - Sm to S8 = 1 without providing details on how the composite data was acquired (Morrow et al. 1985). The work of Amaefule and Handy (1981) in contrast shows that the aqueous phase relative permeability curve changes as the interfacial tension decreases. Similar work conducted by Morrow et al. (1985) showed that reduction in the interfacial tension by an order of magnitude produced no obvious change in the relative permeability. To the knowledge of the author, similar measurements have not been made in unconsolidated natural soils for aqueous phase permeability as a function of trapped residual NAPL or gaseous phase saturations, especially when the residual NAPL saturation is reduced as a result of mass transfer into the aqueous phase. The overall objective of this research was to develop a better understanding of the relative permeability of the aqueous phase characteristic of a region near the capillary fringe contaminated with residual trapped NAPL before and during surfactant treatment. The specific objectives were 1) to measure the saturation of trapped residual dodecane in 62 a naturally occurring unconsolidated porous media as a function of the ratio of viscous and capillary forces; 2) to measure the relative permeability of the aqueous phase in the media as a function of the saturation of trapped residual NAPL; 3) to measure the reduction in relative permeability of the aqueous phase as a function of two trapped residual immiscible phases (NAPL and gaseous phase) simulating conditions that may occur in the capillary fiinge; and 4) to measure the increase in the relative permeability of the aqueous phase as the trapped residual NAPL is reduced by surfactant enhanced dissolution. 5.2 Materials and Methods A borosilicate glass column designed to minimize sorption losses and to maintain a hydrophilic surface (Zalidis et al. 1991) was modified for use in this research (Fig. 3.1). The column was altered for saturated soil experiments by removing the porous pressure plate from the bottom of the column. In addition, the experiments conducted in saturated soil do not require a venting port in the top cap. The column was designed for easy assembly and disassembly. The length of the threaded rods can be changed to accommodate different column lengths. In addition, Viton® o-rings, stainless steel screens and Teflon® caps were used to maintain hydrophilic surfaces which minimize sorption losses. White Ottawa sand obtained from Soiltest (Lake Bluff, Illinois) is used in these experiments (Fig. 3.2) to model homogeneous soil commonly found in sandy aquifers. Deionized deaired water is used to wet the soil column and to prepare surfactant solutions. A nonionic surfactant, Witconol NP-150 (ethoxylated nonylphenol) used as received fi'om “frtco (New York, New York), was used to enhance the aqueous phase solubility of the NAPL. Dodecane from the Phillips 66 Company (Borger, Texas) is used as a surrogate NAPL based on the following desirable physical properties: 1) the specific gravity of dodecane is less than one (LNAPL); 2) low toxicity; 3) very low solubility; and 4) low volatility. The last two properties are necessary to limit the mass 63 transfer between the phases during the experiment consequently allowing the research to focus on the enhanced dissolution of the NAPL into the surfactant enhanced water. To simulate conditions in the upper region of the capillary fringe, a trapped residual immiscible phase was established by flooding a water saturated column with approximately one pore volume of the immiscible phase under 5 psi of pressure, followed by a minimum of 5 pore volumes of water. In some of the columns, a trapped residual gaseous phase was established followed by a trapped residual NAPL phase to simulate condition near the capillary fiinge. A thorough discussion of these methods is presented in Chapter 3. Hydraulic conductivity, K, was measured using the falling head method (Klute 1986) for initial experiments K = (%,)1n(%2) (5.1) where a is the cross sectional area of the standpipe, A the cross sectional area of the soil sample, 1 is time, L is the sample length and H, and H 2 measurements of the initial and final hydraulic head (Fig. 3.2). For the experiment where the relative permeability of the aqueous phase was measured during continuous surfactant pumping, conductivity was measured by the pressure difference across the column using a water manometer K = -—QL AAH (5'2) where Q is the flux rate, L the length of the column and AH the hydraulic head difference across the column (Fig. 3.3). Hydraulic conductivity, K, is a measure of fluid flow through porous media. It is a firnction of both the fluid and soil properties. K: We ,1: (5.3) 64 where k is the permeability of the soil, p is the density of the fluid, 11 is the viscosity of the fluid and g is acceleration due to gravity. In a two— or three-phase system, permeability is also considered to be a firnction of the fluid phase saturations (Section 2.3; Fig. 2.5). The relative permeability, k,, is the permeability scaled by the saturated permeability, km, which in these experiments is the saturated permeability of water prior to surfactant enhancement. K k k = — = — 5.4 ' Ksar km! ( ) 5.3 Results and Discussion Prior to measuring the relative permeability of the aqueous phase at $0 2 1 - Sm, a range of Sm values was measured for the natural unconsolidated soil studied. Experiments were then conducted to measure the relative permeability of the aqueous phase over a range of aqueous phase saturations in this region of discontinuous nonwetting fluid. Additional experiments were also conducted to measure the relative permeability of the aqueous phase in the presence of both trapped residual NAPL and a trapped residual gaseous phase. In these experiments, each data point represents a separate column experiment, assuming that the saturation of the residual trapped NAPL and the trapped residual gaseous phase was uniform. A third experiment was conducted to measure the increase in the relative permeability of the aqueous phase in a single column study as the saturation of the trapped residual NAPL was decreased through the dissolution of the NAPL into a surfactant enhanced aqueous phase. The data was then used to evaluate to existing models for predicting the relative permeability - saturation relationship. 65 5.3.1 Trapped Residual NAPL A range of aqueous phase at $0 2 1 - Sm, were measured by changing the ratio of the capillary to viscous forces, as represented by the capillary number, Ne (Eqn. 2.5) as presented in Table 5.1. Past researchers have estimated that No, needs to be > 10'4 to minimize residual entrapment or mobilize trapped residual NAPL (Wilson et al. 1990; Chatzis and Morrow 1984; Larson et al. 1981). Unless the IFT is reduced, a capillary number this high would requires nondarcian flow rates which are almost never observed in nonindurated rocks and granular material under natural conditions (Freeze and Cherry 1979). The upper limit of Ne within the range of Darcian flow can be estimated by Eqn. 2.5 and Eqn. 3.4 assuming 1< Re <10. < Rey2 Ne- pda (5.5) In Table 5.1, a bulk density of 1.81 i 0.03 (1.5%) and a porosity of 0.39 i 0.01 (3.4%) indicate column packing and initial aqueous phase saturation reproducibility. For the total range of Nc, Sm ranged between 131-36.5%, excluding one unexplainable measurement of 5.1%. The range of Sm is reduced to 136-32.6% if the upper limit of Darcian flow is assumed to be at Re =1. This range is a reflection of the variable ganglia sizes found in Ottawa sand (Powers et al. 1992). Table 2.1 reviews past research in trapped residual NAPL which indicates that a range of trapped residual NAPL can exists in sands. A similar review is presented in Mercer and Cohen (1990). In these experiments, and in past research, the size and the shape of the trapped residual NAPL is assumed to be uniform. However, trapped residual NAPL has been cast in place in sandstone, glass beads and sand, illustrating the wide range of ganglia I ' sizes and shapes, by polymerizing styrene under high temperature and pressure (Chatzis et al. 1983; erson et al. 1990; Powers et al. 1992). A single isolated drop in a pore space can exist within the same region as elongated multiple pore ganglia or ganglia branching throughout a cluster. These blob casts were made from column experiments where the size of the column may have a limiting influence on the size and shape of the larger blobs which may not occur in the field. Hunt et al. (1988) conducted a review of previous work in petroleum engineering and fluid mechanics in NAPL emplacement and mobilization from a different viewpoint. In this review, equations were presented to provide an order of magnitude estimate of the maximum stable length of residual NAPL blobs, also referred to as ganglia, in both the saturated and unsaturated region. The following text summarizes their findings. In the saturated region the maximum vertical length of a ganglia, meax can be estimated by the Hobson Equation (Berg 1975): 20”,, L r. glApl v,max Ill (5.6) In this equation r, is the radius of the smallest constriction of a pore (throat radius), g the gravitational constant, and the interfacial tension between the NAPL and the aqueous phase and Ap the density difference. For horizontal flow, the maximum ganglia length, Lh,max> can be estimated by : 0,0216 203... (5.7) Lt. . .Uav’} Paglrr Ill Ill ,max where k is the permeability of the soil, pa the viscosity of the aqueous phase, v velocity, p a the density of the aqueous phase and i the hydraulic gradient. In the vadose zone, the stable ganglia length, Lv’max, can be estimated as: 2 LW 5 ”"8 (5.8) r. p. g where ong is the interfacial tension between the NAPL and the gaseous phase and p" is the density of the NAPL. The radius of the throat (r,) may be estimated fi'om a rhombohedral packing of a spherical media with a diameter d (Berg 1975): ' 67 r, z 0. 077d (5.9) Using the soil and fluid properties in Table 5.2, these equations were used to provide an order of magnitude estimate for the maximum size of a stable trapped residual ganglia of NAPL, hence predicting the potential for a large range of ganglia sizes and shapes Since Nb > 0.00667 (Sec. 2.2; Fig. 2.3), No can be used to estimate the trapped residual volume of NAPL prior to surfactant injection. Typical flow rates in sand and gravel aquifers range from 10m/y to 100 m/y (3 x 10'5 cm/s to 3 x 10‘4 cm/s) (Mackay et al. 1985), resulting in 6 x 10'9 3 Ne _<_ 6 x 10's. The maximum vertical stable ganglia length in the saturated region is estimated at 112 cm., whereas the maximum horizontal stable ganglia length is estimated between 90 - 900 m. For the vadose zone, the maximum stable vertical ganglia length is estimated at 18 cm. It is reasonable for hydrological cycles to drop the water table greater than 18 cm., resulting in such an elongated ganglia (i.e., in Reichmuth 1984 the water table fluctuated 142 cm. between September and February due to seasonal recharge/discharge). When the water table rises, these ganglia will be captured in the saturated region. Calculations support that these ganglia are well below stable vertical lengths for the saturated region. As a result, a rising » water table will not mobilize these ganglia. When estimating the maximum horizontal stable length in the saturated region as a function of gradients, a 1% gradient (i = 0.01) can trap a stable ganglia 27 m long whereas a 10% gradient can maintain a stable ganglia length of 3 m. This explains in part why pump and treat technology has limited use in the remediation of LNAPL. When a drawdone cone develops in the are of a pumping well, a portion of the pool of LNAPL will migrate under the influence of the locally steep gradients. These calculations predict that stable ganglia can remain trapped over a large region as opposed to reaching the well where the NAPL can be removed. As stated previously, in the saturated region it is estimated that 10-50% of the pore space is saturated with trapped residual NAPL ganglia. 68 As stated, these estimates only provide an order of magnitude estimate for the maximum stable ganglia lengths. Much smaller lengths were found in the polymerized styrene blobs, which at the most extended over a few pore spaces. The purpose of evaluating the stable ganglia length was to suggest that trapped residual NAPL saturations in the field may be significantly higher locally, resulting in significantly higher reductions in the relative permeability of the aqueous phase. Column experiments provide a better understanding of the saturation-permeability relationship in the range measured, but it is not clear it adequately describes the in-situ environment without further exploring 2-D and 3-D situations. 5.3.2 Reduced Permeability Of the Aqueous Phase Due to Trapped Residual Phases In order to simulate conditions in the upper region of the capillary fiinge, water saturated columns were flushed with air followed by water to trapped residual air phase. The trapped residual immiscible phase reduced the relative aqueous phase conductivity to 0.63 i 0.04 (Fig. 5.1). Morrow et al. (1988) reported that the relative permeabilities for bead packs were largely independent of establishing the residual saturation by mobilization or entrapment and the phase of the trapped residual (e.g., gaseous phase or oil phase). Therefore, the reduction in relative permeability may also represent a region within the capillary fringe or below the water table where trapped residual NAPL only is trapped. Trapped residual air saturations were measured between 11.27-15. 14% (average 13.6; standard deviation 4.5), which is consistent with the saturation of NAPL measured previously. The columns were then flooded with NAPL, followed by a water flush to establish a trapped residual NAPL phase in addition to the trapped residual air phase. The trapped residual air is largely in the larger pore spaces prior to the NAPL infiltrating the column. Trapped residual NAPL saturations were estimated based on the assumption that the trapped residual air phase remained within the soil matrix. Between 4-30% (average 17.43; standard deviation 8.5) of the pore space was occupied by a 69 trapped residual NAPL, reducing the relative permeability of the aqueous phase to 0.32 i .02 (:1: 6%). Experiments were also conducted with only NAPL trapped as a residual immiscible fluid. In these experiments, the aqueous phase saturation was reduced to 69.6-84.5% (average 80.1; standard deviation 5.1) . As a result, the relative permeability of the aqueous phase was reduced to 0.52-0.74 (average 0.6; standard deviation 0.08). These results are comparable to a reduction in the relative permeability of the aqueous phase to 0.6 when a trapped residual air phase was established in the water saturated I column, although the range of saturation for the trapped residual NAPL only is slightly larger. 5.3.3 Aqueous Phase Permeability During Surfactant Enhanced Dissolution of NAPL A trapped residual NAPL phase saturation of 17.9% was established in a soil column followed by continuous injection of 5% solution of Witconol NP-150 for 14 days. The relative permeability of the aqueous phase was measured as a function of pore volumes by monitoring the head loss across the soil column using a water manometer. The results indicate that the trapped residual NAPL reduced the relative permeability of the aqueous phase to 0.52. The initial surfactant injection firrther reduced the relative permeability of the aqueous phase to 0.35 which indicates that the viscosity and density of the surfactant is different that deionized water used to meaure the conductivity previously. After 14 days of continuous pumping, the relative permeability of the aqueous phase increased to 0.58. A final flush of 4 pore volumes water further increased the permeability to 0.92. Surfactant injection without trapped residual NAPL reduces the aqueous phase relative permeability to 0.78, which again indicates a difference in the viscosity and density of the surfactant compared to the deionized water used to measure the saturated conductivity. The final flush of water may not have completely removed all of the surfactant which would result in a lower aqueous permeability as well as a lower 70 weight measurement for the final determination of NAPL removal, since the density of surfactant is less than the density of water (Table 5.4). Weight measurements estimated a complete removal of the NAPL although further pulsed pumping of surfactant indicated filrther NAPL removal. If the remediation design was based on pumping surfactant into a contaminated region without consideration for the reduced flow within the region of reduced conductivity, the estimated flow into the region of contamination would have been in error since flow into the contaminated region is reduced to approximately 52% by the method of Wheatfield and Winterberg. Toward the end of the treatment, the flow had increased to 73%. This range of reduced flow, although estimated on the basis of an idealized homogeneous uniform flow, suggests that pumping strategies should account for reduced permeability that will increase over time in order to develop an economical remediation technology. This experiment was conducted in a naturally occuring unconsolidated soil as opposed to consolidated sand stone or glass beads common research conducted for petroleum reservoirs. It is also unique in that the data is collected continuously in a single column as opposed to collected data over a series of column experiments where the distribution of the trapped residual non-wetting phase or soil packing may vary. The data follows the trend of the data collected in the previous sets of experiments, indicating that the final combined graph can be used to predict the permeability regions near the capillary fiinge for the aquifer material studied. 5.3.4 Comparing Data in Discontinuous Region with Existing Fitting Parameters Figure 5.2 contains data derived from a series of experiments where the range of trapped residual NAPL saturation measured in an unconsolidated porous media was varied by changing the ratio of the viscous and capillary forces. In addition, data is 71 included from an experiment where the trapped residual NAPL was reduced through dissolution into a surfactant enhanced aqueous phase. A discussion of the relative permeability-saturation curves is presented in Sec. 2.3 which describes the 2-phase relationship in detail. Empirical equations have been developed based on experimentally derived coefficients or fitting parameters A, 01', n’ and m for both pressure-saturation relationships and relative permeability-saturation relationships. Corey (1986) defines these relationships as a function A and effective saturation (Se) of the aqueous phase. 11 S, =Sl—“__S—SM-=(%) (5.10) km = Sf?" (5.11) where S0 is the saturation of the aqueous phase, Sm the residual or irreducible saturation of the aqueoUs phase, 11,, the displacement pressure head, It pressure head, and km the relative permeability of the aqueous phase. Van Genuchten (1980) defines these relationships using 0', n' and m: _&—&~ 1 ” S" l-Sm :(1+(ah,)") (5'12) km =S}{1—[1—S,‘i5)]"} (5.13) where he is the capillary pressure. head. It is usually assumed that m = 1-1/n'. Both 11' and 1 are measures related to the pore size distribution index such that n' = 2. + 1 (Powers et al 1992; van Genuchten, 1980). Table 5.1 summarizes values of A, 01', n' and m reported in the literature for Ottawa sand. Soeryantono et al. (1994) used the same soil analyzed throughout this research. Powers et al. (1992) used a 20-30 mesh Ottawa sand purchased from Fischer 72 Chemical Co. In both works, the fitting parameters were derived from data measuring the pressure-saturation relationship. In Figures 5.4-5.8, the fitting parameters for both Corey's and van Genuchten‘s relationships were used to estimate the relative permeability saturation relationship in the region where both the wetting and non-wetting fluids are continuous. The curves were then extended into the region where the non-wetting fluid is trapped over a range of trapped residual non-wetting saturations using the same equations and fitting parameters. The irreducible aqueous phase saturation (Sm = 0.093) was measured by Soeryantono et al. (1994) from the same Ottawa sand used in this research. Figures 5.4-5.6 use the fitting pararnetes measured by Soeryantono et al. (1994) over the range of possible values (e.g., A = 2.32 :t 0.02; n' = 4.27 i 2.72) Powers et al. (1992) values for imbibition and drainage are presented in Figures 5.7-5.8. In all cases except the use of the van Genuchten parameters in Figure 5.4, the extended curves predicts the trend in the lower region of the data to some degree. However, none of the curves describe the data in the upper region. The curves do predict that a small change in the saturation of the trapped residual non-wetting phase results in a larger change in relative aqueous phase permeability compared to the regions where the nonwetting phase was continuous. The results indicate that the existing fitting parameters do not adequately predict the permeability-saturation relationship in the region of interest. Therefore, the raw data may need to be used directly in design and modeling pumping strategies in this research. 5 .4 Summary Experiments were conducted to measure the relationship between the relative permeability of the aqueous phase and the aqueous phase saturation in a two-phase system where the nonwetting phase is discontinuous. Over a range of trapped residual nonwetting saturations between 11.27-15.14% the relative aqueous phase permeability was reduced between 0.6k,. to 0.8/tr. The range of trapped residual nonwetting phase 73 saturation was established by varying the ratio of the viscous to capillary forces. Similar studies have been conducted by petroleum engineers in sandstone and glass beads, but to the knowledge of the author, this study is unique in that it was conducted for a naturally occuring unconsolidated soil. The study was extended to measure the relative permeability of the aqueous phase with both a trapped residual NAPL and a trapped residual air phase established. Using the columns from the previous set of experiments where trapped residual air saturations were measured between 11.27-15.14%, an additional trapped residual NAPL was established between 4-30% saturation. The combined trapped residuals reduced the aqueous phase to approximately 0.32k,.. In the research conducted by the petroleum engineers, this type of experiment provided a measure of the relative permeability of the aqueous phase in the region of trapped residual NAPL but also provided a measure of pressure gradients or reduction of interfacial tension needed to decrease trapping during water flooding or increase mobilization of the trapped residual NAPL. The pressure gradients needed to decrease the amount of trapping in groundwater aquifers are unrealistic. Releasing trapped residual NAPL by reducing the interfacial tension threatens to spread the contaminant further through the aquifer. This research considers the use of a surfactant to enhance the solubility of the trapped residual NAPL into the aqueous phase. While many in-situ remediation requires a measure of the reduced permeability in the contaminated region, the dissolution of the trapped residual NAPL requires a measure of the increasing aqueous phase permeability over time. An initial design based on promoting both the flow through a contaminated region of reduced aqueous phase permeability and the contact time needed for optimizing the solubility of the NAPL may need to be modified as the flow paths change due to the reduced saturation of the trapped residual NAPL and a concurrent increase in the relative permeability of the aqueous phase. Under constant head boundary conditions, the increase in permeability will result in an increased aqueous flow into the contaminated region. Under constant flux boundary conditions, the 74 increased permeability will result in an increase contact time of the surfactant enhanced aqueous phase (Wilson et al. 1990). An additional column experiment was conducted to measure this relationship. In addition to providing the design parameters needed for this research, this experiment is a unique approach to measuring the permeability-saturation relationship in the region considered. One may argue that in an actual sandy aquifer targeted for remediation, the reduced relative permability in the contaminated region due to trapped residual NAPL may be minor when considering local heterogeneities, such as silt or clay strata, which may reduce the permeability by a factor of 1000 to 10 million (Mackay and Cherry 1989). In groundwater aquifers, capillary forces are generally stronger than the combined viscous or buoyance forces. As a result, NAPL will be trapped in the larger pores of a sandy region as opposed to migrating or trapping in the smaller pores in the less permeable regions. The clay and silt layers may provide regions within the aquifer which locally represent an confined aquifer promoting flow into a contaminated lens of soil, while causing unpredicted surfactant by-passing in another area. The size and shape of the contaminated region relative to the size and shape of the region of clay or silt needs to be considered when characterizing the region and evaluating the use of hydraulic controls to efficiently deliver, recover and promote surfactant enhanced dissolution. 75 0.9 -- 0.8 *- 0.7 -~ g *4 _ O 0'6 , 9 Trapped residual air .. O O Trapped residual air and oil RELATIVE PERMEABILITY .6 .c .<= .o N U A M i l l i O 0 <6) 0 .O a—s 1 l 0 i i i i i i i i i l 0 10 20 3O 40 50 6O 70 80 90 100 AQUEOUS PHASE SATURATION (%) Figure 5.1. Measured values of relative permeability and saturation of the aqueous phase with trapped residual air and trapped residual oil. 76 l .... 0.8 ~ g 4 k1 OnesidunlExp. : h 06 .0. ODissohm'onExp. .? ' 4 E a «so 3 83: a 0.4 r o H 8 S . At ‘8 o 0.2 ~~ rd :3 O < O 1 i i i 4 0 0.2 0.4 0.6 0.8 l AQUEOUS PHASE SATURATION Figure 5.2. Aqueous phase relative permeability as residual NAPL is reduced through surfactant enhanced dissolution. A 3.5- a l r. 3.45 " E 3. . 0 > g 3'35 ‘ W00 3 3.3 . ° . - - - 0 0.2 0.4 0.6 0.8 1 Relative Permeability Figure 5.3. Error associated with relative permeability measurements. .63 u ..H .8." u «...H... v «.8... ..H 5:233. 3.2..— 3323 ..H—.28.. a 5; 3a.... 282:3 2: .3 35:83.9. =2.§5a?bm=aao::2_ 9529.. 2: .8.— ..85556 S; can .380 .3 335.8.— ..8595 8 8a.. aura—.50 in flawfi 77 zofigé mam: 38:3 20:55 mafia 88:3 m wd ed v.0 «.9 Q ~ wd 0.6 #6 N6 o w n H ...H ........ n o T \ ....H ....... n c m m m m ., do m ., 3 m S S W O .d S 9..... M -, to m o... -. to m w M. m. 32.3: o u w . Spas: 0 u 3 -. H; m 9 ..H... .- 2H m 8535 0 M. Q Sneeze O m...“ 5209185 ....................... m 0 F5385 ....................... M 638605» 11 we W 62860.! lac W m m l — l m .5... u ..H .8." u 2:5: V «.85 ...H 5:23am 85... 252:3 1328.. a 5m? 82:. 232...: 2: .3 3:28:22 =o:a..3a?b=3ao::on 3:29.. 2: .8.— ..ofioasmv =5» .25 .380 ..o 3.3—:8 :32an 8 3a: wctanEoU .m.m 9..—arm 78 zofifispé mafia 88:3 zoPfiSSm mafia 8953 H 3 9o EH 3 o _ no 3 EH 3 o 1.-» » o » » »1..».. + o P h F u « 0 0...... w .96 2&5. O Q .~ ,9 .1 ed .3 r 9o O 53335 O ....................... 3.60.385 % wd fizuauoglll .1 wd ALI'IIHVEIWHEH ElAILV’IEl‘d ElSVHd snoanbv wnavamad HALLV’IERI EIS'v'Hd snoanbv .83 n ..H .3." u 3...... v 3...: 2 8:82.23 82:. 282:8 8:28.. a _:_3 82..— 8853 2: .8 3:88:29. 8:588?b=33=:2_ 3:50.. 2: .8.— .822890 E; .28 .380 .8 8888:3188». 8 52. 2:89.80 9m 082m 79 zoESHPSHm mafia 8089. 205233 ESE 3859. H no we ...H. 3 o H 3 3 to S o p u «L- T4»- ‘. #- 0 4p p—o— o ‘V" b q u 1 l N. O l l N. O l l V. o l l ‘5! o 1 l °°. o umavawuad HALLV'IEDI EISVHd snoanbv umavamad HALLV'Izm ElSVHd snoanbv .93. u ..H .3." u 2:5. » n8... 2 8:988» 8228 282:8 8:28.. a .:_.$ 3.28 2.82.8 2: .8 3:28:22 =3:E=8?b=338.8: 3:50.. 2: 8.. 282.2289 28> .28 .880 .8 888.8.— ..32828 8 «22. 8:22.80 Em 9.82m 80 zoFSSEm was: gonzo... 885% as: 8859. H 3 3. ...H. 3 o H no 9o 8 S o _ O F _ L b _ o H q H H H l l N. o l l “l o O O % ..me 2E5 0 a. .. O 1 9o ...... 1 9o O 8:230 O ....................... in 1r ”.0 52350:!l .... w.o mmavawaad ElAIlV’IERI EISVHd snoanbv umavawuad EIAIlV'IEI‘d aSVHd snoanbv A": u ..H .21... u 3...... v «.25 2 8:988... 0228 88:8 8:38.. a :23 8228 88:8 2: 8 2:88:29. 8:8:8»-§_E8E8: 3:28.. 2: .8.— .828280 28> :8 8.80 .8 22:88.— _8:_:Eo 3 :8: wing—80 .w.m 8.82.: 81 20:55 as: 2883 2053593 mmsa 88:9. H no 8 to No o H no we ...o No o .r » H ........ » o H H » H ......... H o V V O O m m 1: NO m 1: No m w. m 0 , 3H N» Am to m» m ......_ . v w u w .3385 O u H- 8 m Q .3 .- 9o m mm ” 89:08.0 0 mm m 0 8.80.385 ....................... m 1: ”.0 W fiEoBBOEll i ”.0 W H". m » w M - H .- H 82 Nc Error Sm Error Relative Darcy Re pd n Error(%) velocity’ (ml/min) 2.46E-04 1.231504 0.365 0.008 0.021 0.635 2.678 ND 1.789 0.402 1.64E-03 8.22E-04 0.365 0.008 0.021 4.232 17.859 ND 1.801 0.401 2.45E-04 1.231304 0.131 0.003 0.026 0.635 2.678 ND 1.766 0.403 1.65E-03 8.26E-04 0.204 0.005 0.023 4.232 17.859 ND 1.792 0.399 3.30E-06 20413-06 0.165 0.004 0.024 0.008 0.035 D 1.818 0.389 6.75E-04 3.37E-04 0.154 0.004 0.025 1.693 7.143 ND 1.822 0.390 3. 1913-06 1.98E-06 0.172 0.004 0.024 0.008 0.035 D 1.792 0.402 2.43E-05 1.22E-05 0.247 0.005 0.022 0.063 0.267 D 1.801 0.405 2.68E-05 1.35E-05 0.326 0.008 0.025 0.063 0.267 D 1.833 0.364 2.29E-03 1.15E-03 0.051 0.002 0.044 5.925 25.003 ND 1.770 0.402 7.09E-05 3.55E-05 0.201 0.005 0.023 0.169 0.713 D 1.835 0.371 1.06E-04 5.291305 0.136 0.004 0.026 0.254 1.071 D 1.854 0.373 6.8013-05 3.40E-05 0.179 0.004 0.024 0.169 0.713 D 1.839 0.387 2.91E-06 1.461506 0.145 0.004 0.030 0.169 0.713 D 1.778 0.389 1.807 0.391 avg D=darcian 0.027 0.013 std ND=nondarcian ‘ flushing velocity 1.520 3.409 cv(%) Table 5.1. Capillary number vs. saturation. 83 Parameter Value Method d 0.05 cm d50; sieve analysis Pn 0.748 :1: 0.0003 g/cm3 measured 25°C Pa 0.998 :1: 0.0004 g/cm3 measured 25°C ps 0.995 :1: 0.0032 g/cm3 measured 25°C °na 52.8 :t 0.2 dynes/cm 25°C; Johnson and Dettre 1966 . Orig 24.9 :t 0.2 dynes/cm 25°C; Johnson and Dettre 1966 °ns 3.73 :t 0.09 dynes/cm 25°C; Pendant Drop Method pa 0.01 poise 20°C; Potter and Wiggert 1991 k 10*5 cm2 Freeze and Cheny 1979 Subscripts Aqueous phase (deionized water) NAPL (dodecane) Gaseous phase (air) Surfactant (5% W i tconol NP- 150) Table 5.2. Soil and fluid properties. 84 Minimum Maximum Wetting phase NAPL Flow Rate 3 x 10'5 cm/s 3 x 10‘4 cm/s water dodecane Nb 2.9 x 10‘5 n/a water dodecane Nc 6 x 10-9 6 x 10-8 water dodecane Lv,max saturated 112 cm n/a water dodecane Lh,max saturated (1) 900 m 90 m water dodecane Lh,max saturated (2) 27 m n/a water dodecane Lh,max saturated (3) 3 m n/a water dodecane Luna: unsaturated 18 cm n/a water dodecane Lh,max saturated (1) 63 m 6 m 5% Witconol NP-150 dodecane Nb 0.04 Na 5% Witconol NP-lSO dodecane Nc 8 x 10'8 8 x 10‘7 5% Witconol NP-150 dodecane (1)estimated from velocity (2)estimated from gradient i = 0.01 (”estimated from gradient 1 = 0.1 Table 5.3. Order of magnitude estimate for ganglia size 85 Parameter Value Source a'i 0.222 Powers et al. 1992 “'d 0.094 Powers et al. 1992 n'i 3.58 Powers et al. 1992 n'd 7.42 Powers et al. 1992 n' 4.27 :l: 2.72 Soeryantono et al. 1994 11' 2.30 Powers et al. 1992 id 3.46 Powers et al. 1992 3. 2.32 :t 0.02 Soeryantono et al. 1994 Table 5.4. Reported values of fitting parameters for white Ottawa sand used in relative permeability-saturation and capillary pressure-saturation relationships in a 2-phase system (i = imbibition; d = drainage). Chapter 6 Numerical Modeling 6.1 Introduction Leaking underground storage tanks, illegal disposal of waste and pipeline ruptures results in subsurface spills of nonaqueous phase liquids (NAPLs) which contaminate the groundwater. As NAPL migrates through the soil matrix under the influence of capillary, viscous and buoyancy forces, a residual saturation of NAPL will remain in the pore spaces. In the unsaturated region, residual NAPL has been traditionally viewed as a continuous film between the aqueous and gaseous phase present in the pore spaces. However, recent flow visualization experiments conducted in micromodels suggest that nonspreading NAPLs may actually coalesce as discontinuous ganglia on the aqueous phase interface (Wilson 1994). Larger spills which are not completely reduced as residual in the vadose zone will pool above the largely water saturated pores of the capillary fringe until sufficient pressure is developed to drain the aqueous phase from the pores. NAPL less dense than water (LNAPL) such as natural and refined hydrocarbons (Knox and Sabitini 1991) will continue to pool while slightly depressing the capillary fringe. Seasonal watertable fluctuations or plume migration due to natural gradients can cause this pool of NAPL to become discontinuous and immobile as a trapped residual phase. NAPLs more dense than water (DNAPL) such as chlorinated organics and solvents (Knox and Sabitini 1991) will migrate through the capillary fiinge. The migration of DNAPL will continue through the saturated region until it is completely exhausted as a discontinuous and immobile trapped residual phase or pooled above less permeable strata in the aquifer. Despite the reduced saturation of residual NAPL remaining in the pore 86 87 spaces, it creates a long term source of pollution partitioning slowly into the aqueous and vapor phases (Schwille 1988; Mackay et al. 1985). Trapped residual NAPL is considered one of the major limitations to conventional pump-and-treat technology (Schmelling 1992; Hall 1989). The chemical enhancement of pump-and-treat methods with surfactants and cosolvents has been studied to improve the technology (i.e. Ellis et al. 1985; Nash 1988; Abdul et al. 1992; Clarke et al. 1992; Pennell et al. 1993; Fountain 1991). In a 1992 report , the Environmental Protection Agency identified key areas of concern for chemical enhancement of pump-and-treat remediation which include as the delivery of the reactive agent to areas of the aquifer where it is needed and the removal of the reactive agent from the subsurface (Palmer and Fish 1992). NAPL blocks or reduces the flow of the aqueous phase into the contaminated region. This in part explains why the limited number of field applications to date of in- situ remediation technologies for the treatment of NAPL have not achieved the high efficiency suggested by 1-D column experiments (Ellis et al. 1984; Nash and Traver 1984; Nash 1985). The columns impose an artificial boundary which controls fluid movement between injection and recovery points. However, in the field flow is free to by-pass the NAPL contaminated region due to the resistance caused by this immiscible phase within the soil pores. This resistance can be decreased if the NAPL saturation is reduced through pumping or natural plume migration. The remaining discontinuous residual saturation is far more difficult to remove, trapped by capillary forces stronger than the combined opposing viscous and buoyant forces. In the saturated region, residual NAPL occupies between 10-50% of the pore space (Wilson and Conrad 1984). Hence, the pore blockage resisting flow is still significant. The problems caused by blockage are accentuated in the capillary fiinge, where a residual gaseous phase is also trapped within the soil pores, fiirther reducing the aqueous phase permeability. 88 Field data and column studies have shown that the extent of interphase mass transfer from the NAPL to the aqueous phase are limited by chemical or physical processes (Power et al. 1992; Mackay et al. 1985; Mercer and Cohen 1990; Miller et al. 1990). Powers et al. (1992) suggests that these limitations are due to: 1) rate-limited interphase mass transfer (nonequilibrium); 2) physical bypassing of the mobile aqueous phase around contaminated regions due to relative permeability effects or aquifer heterogeneities; and 3) dependence of equilibrium solubilities on NAPL composition. Equilibrium mass transfer assumes that the maximum solubility of NAPL into the surfactant enhanced groundwater will occur instantly. Rate-limited interphase mass transfer may result in less than predicted removal rates if the time needed to promote the maximum solubility of NAPL into the surfactant is not achieved between the injection and recovery wells. In contrast, continuing to pump surfactant which has reached the maximum solubility of NAPL through a polluted region is justifiably as inefficient. Less than optimal interphase mass transfer may also be a result of in-situ physical limitation. In the complex network of pores spaces within the soil, trapped residual NAPL may be isolated as a single blob or branched through several pores spaces. As a result, the solubility of NAPL into the surfactant enhanced groundwater may be limited at the pore scale by dead end pore spaces or groups of blob blocking flow , restricting flow or reducing the contact area for mass transfer. As the surfactant enhanced aqueous phase reduces the NAPL saturation through dissolution, the permeability will increase within the region. Under constant head boundary conditions, the increase in permeability will result in an increased aqueous phase flow into the contaminated region. Under constant flux boundary conditions, the increased permeability will result in an increase contact time of the surfactant enhanced aqueous phase within the contaminated region (Wilson et a1. 1990). As a result, the economical and efficient use of surfactants to enhance the dissolution of NAPL requires coupling the accurate prediction of rate-limited mass transfer as well as the relative 89 permeability of the continuous aqueous phase over time. This research will incorporate previous 1-D column experiments designed to investigate these to phenomenon in a 2—D study. 6.2 Objective The overall objective of the research will be to evaluate hydraulic controls to promote the efficient use of surfactants to enhance the dissolution of trapped residual NAPL near the capillary fiinge. The specific objectives are 1) to develop an implicit numerical transport code to optimize the pumping rates in a nondimensional l-D study; 2) to evaluate the use of the USGS model SUTRA (Saturated-Unsaturated Transport Model; Voss 1984) to model a vertical cross section of an aquifer which includes the vadose and saturated regions; 3) use SUTRA to predict the capture zone and contact times established by hydraulic controls (i.e. pumping rates and well placement) in a region near the capillary fiinge where the relative permeability of the aqueous phase is reduced due to a trapped residual NAPL; and 4) to evaluate the effects of increased permeability due to dissolution within the region on the design of the system. Column studies have been conducted to measure the kinetics of rate-limited mass transfer and reduced permeability due to trapped residual NAPL near the capillary fringe. In these experiments, a 5% solution of a nonionic surfactant, Witconol NP-150 (ethoxylated nonylphenol) was injected into Ottawa sand with trapped residual dodecane (Chapter 4). The column studies have shown the presence of mass transfer limitations, but the kinetics are not prohibitively slow. A contact time of 12 hr. is needed to achieve the maximum dissolution in the porous matrix of NAPL into a 5% solution of Witconol NP-150. Trapped residual NAPL reduces the aqueous phase permeability by approximately 30%. However, at the capillary fiinge, the gaseous phase can also be trapped as a discontinuous phase, firrther reducing the aqueous phase permeability by approximately 50%. The 1-D column studies also measured changes in the mass transfer over time as the contact area of the NAPL changed in response to dissolution. The column studies also measured the increase in relative permeability as the trapped residual NAPL saturation was reduced by the surfactant. This research will use the data from the 1-D experiments to continue the study of surfactant enhanced aquifer remediation in a 2-D environment. 6.3 1-D Model Development The numerical evaluation will consider a single component NAPL present at trapped residual saturations. The immobilized ganglia are uniformly distributed in a saturated, homogeneous isotropic aquifer material. NAPL transport into the aqueous phase can be predicted by the 1-D advection dispersion reaction (ADR) equation for a homogeneous medium with steady flow in the x—direction: 5C 32C 5C —-=D — —- J 6.1 51 6x2 v§x+ ( ) In the ADR equation, C is the concentration of the solute, t is time, D is the dispersion coefficient, v is velocity, x is distance and J describes the nonadvective flux or dissolution of NAPL into the aqueous phase. Assuming that mass transfer is adequately described by a linear driving force model, J can be modeled as the product of a lumped mass transfer coefficient, k,, the difference in the equilibrium concentration of the solute in the aqueous phase, CS, and the concentration of the solute present in the aqueous Phase C: J = k, (C, - C) (6.2) The reduction of the immobilized ganglia is estimated from the mass balance: ac” a: = -k,(C, — c) (6.3) where C N is the concentration of the NAPL. 91 An implicit numerical transport model (Chapra and Canale 1988; Wang and Anderson 1982) was developed using centered finite divided difference for the spatial terms and block centered nodes, resulting in a tridiagonal matrix. The concentration at a node is weighted over time by a) . CviH-l _ Ci, : 0D Cull-:11 _ 2Cil+l + Cilj-ll + (1 _ (0)0 le+1 _ 2C: + (Iii—1 Ar sz A x2 1+1 _ 7+1 1 _ I — wvgliL—gl— - (1 — co)v——C’+1 C” (6.4) 2Ax ZAX + wk,(C. — Cf“) +(1- w )k, (C. -C.-’) The subscript refers to the x-location whereas the superscript references time. The numerical code was written in FORTRAN. Simulation were performed on an IBM compatible 386/486 computer using a 32-bit compiler. The model assumes that the NAPL is a nonwetting fluid. Consequently, the wetting fluid, in this case the aqueous phase, acts as a barrier to direct contact between NAPL and soil particles, strongly inhibiting the mass exchange which may occur between the NAPL and the soil or solid phase. Prior to surfactant treatment, the trapped residual NAPL is assumed to be uniformly distributed throughout the matrix. Over time, the distribution will become less uniform as a result of the stronger driving force of the nonadvective flux term at the influent end. The aqueous phase solubility of the NAPL is assumed to be low enough that the solute concentration does not affect the density of the contaminated aqueous phase. To minimize numerical dispersion, time was discretized to maintain the Courant (Cr) number less than or equal to one: ' Jfl Ax Cr 3 l (6.5) and the size of the grid met the criteria for the grid Péchlet number: 92 Ax 3 4a (6.6) where or is the dispersivity of the solute (Anderson and Woessner 1992). An analytical solution (van Genuchten and Alves 1982) was used to verify the code during early time when the saturation of the trapped residual NAPL is relatively uniform and constant. The analytical solution for a semi-infinite column exists with a first order decay term and a zero order production term for the following boundary conditions. C(x,0) = C, C(O, r) = C, 0 < r s to (6.7) é’C(oo,t) at For the system under consideration, C0 , the initial concentration of NAPL in the injected surfactant, and C,- , the concentration of NAPL in the aqueous phase present in the soil matrix, are both zero. The solution assumes that the dissolution of NAPL into the aqueous phase begins at time to for all elements and that the surfactant concentration of the aqueous phase is constant. The complete analytical solution is in Appendix A. The 1-D ADR equation can be transformed to a nondimensional form by defining the following dimensionless terms. X:i Daz-ki L v C=£ Fe:£ (6.8) C, D t*=’—" L The nondimensionalized equation becomes 6C 162C 6C =— —— D l-C 6.9 av Peax2 ax+ a( ) ( ) 93 In this equation, Pe is the Péchlet number which represents the ratio of the advection rate to the dispersion rate. Do is the Damkohler number which represents the ratio of the mass transfer rate to the advection rate. The maximum and minimum relative error (emax , 8mm) of the implicit transport code was evaluated from the analytical solution for the soil and fluid characteristics listed Table 6.1 where: Canalyn'cal _ C'implict model .100 (6.10) g : I Canalytr‘cal Figure 6.1 compares the implicit transport numerical code to the analytical solution for a 15 cm column, with a spatial grid of 0.5 cm, Da of 1, Cr of 0.5 and a 0) value of 0.5. In this study, the concentration of NAPL in the surfactant enhanced aqueous phase predicted by the analytical solution and the numerical code were compared at increments through the column. The results indicate that the numerical code can be used to predicted surfactant enhanced dissolution of the trapped residual NAPL. The code was also evaluated to minimize the error between the numerical code and the analytical solution over a range of Cr, 0) and Da to further evaluate its applicability. The first of these studies focused on evaluating the model over a range of velocities. In this study, the velocity was varied while maintaining constant values of Cr = 0.3, L = 15 cm, Ax = 1 cm, 0) = 0.6 and k, = 0.397 hr'l. Since the velocity is a factor in both Cr and Da, At was varied to maintain a constant Cr and 0.5 3 Ba 5100). The results of this study are shown in Figure 6.2. The maximum relative error of 7.48% occurred at Da = 50, whereas a minimum relative error of 0.004% occurred for Da = 0.01. These results suggests that the model can be used over a range of velocities. The evaluation was extended to evaluate the error over a range of weighting values (0.55 co $1) and a range of Cr (0.3 3 Cr 3 0.7). Figure 6.3 summarizes the maximum relative errors found in these studies. From this figure, the maximum error is 94 shown to be minimized (5.58%) at a or value of 0.6 and a Cr of 0.3. As a result, these values will be used in further simulation studies using the 1-D implicit transport model. Two further studies were conducted in order to evaluate the use of the implicit transport model for a wider range of Da with respect to various mass transfer coeflicients and Fe with respect to a range of dispersivity values. Table 6.2 lists a range of k1 measured in other studies which assumed that the mass transfer is adequately described by the same linear driving force model (Borden and Kao 1992; Priddle and MacQuarrie 1994). Using an average interstitial velocity representative of naturally occurring velocities in sandy aquifers (v = 0.1 cm/min) and a higher velocity representative of low flow pumping conditions (v = 1 cm/min), the maximum and minimum error between the numerical code and analytical solution was predicted for this range of k,. The system was evaluated at a length of 15 cm, spatial discretization of 1 cm, a Cr of 0.3 and a 0) value of 0.6 while assuming a constant value of dispersion. The maximum relative error is below 4.27% for Do < 100 (Fig. 6.4). However, when the values of dispersivity were varied for naturally occurring aquifer material (Mercer et al. 1982) resulting in 10'2 < Pe < 104, much larger errors are present (Fig. 6.5) for the same conditions, assuming a constant k, of 0.387 hr'l. If the acceptable maximum error is 10%, this study suggest that this model may be limited to Fe 3': 100. A firrther optimization study could be conducted which may determine that different values of Ax, co and the Cr decrease this error. However, the objective of this study is to evaluate the dissolution of a single component of gasoline (dodecane) into a nonionic surfactant (5% Witconol NP-l 50) fi'om a sandy aquifer material. As such, error analysis of the code will only consider optimizing these values with respect this study. Two early versions of the 1-D transport model developed evaluated the use of an explicit scheme using both the Quick formulation (Leonard 1979) and a centered finite divided difference approximation for the advection term. In both codes, the centered finite divided difference approximation was used for the dispersion term. A fixed step 95 size 4th order Runge Kutta method was employed to solve the resulting ordinary differential equation. Semprini and McCarty (1991) report problems with the Quick Method near the influent end when high concentration accumulated. The increase driving force of dissolution at this end for the system modeled resulted in errors which may be similar. The centered finite divided difference approximation of the advection term resulted in large oscillations around an average value at later time. 6.4 Simulation Studies Using l-D Implicit Transport Model The 1-D implicit transport model was developed to predicted the behavior of a nonionic surfactant (5% Witconol NP-ISO) which enhances the solubilization of trapped residual NAPL into the aqueous phase. The numerical code was compared to an analytical solution to evaluate the minimum and maximum relative error during early pumping, assuming that the distribution of trapped residual NAPL remains relatively uniform. However, the dissolution of NAPL into the surfactant enhanced aqueous phase is a rate-limited process which results in an uneven distribution of trapped residual NAPL in the column over time, limiting the use of the analytical model. Figure 6.6 illustrates the removal of NAPL over the column length at specified pore volumes (2, 20, 40, 60) using the implicit transport model for Cr = 0.3, 0) = 0.6, Da = 10, L = 15 cm and Ax = 1 cm. Clean-up occurs more rapidly at the influent end resulting in an uneven distribution of trapped residual NAPL remaining in the soil as the remediation progresses. Figures 6.7- 6.8 show similar results for the same conditions but at a higher velocity (Da = 1) and a lower velocity (Da = 100). Changing the velocity decreases or increases the residence time of the surfactant. However, the stronger removal at the emuent end is still evident. Figure 6.9 illustrates the mass transfer over time by solving the ordinary differential equation in Eqn. 6.2 for no flow conditions. x— — _ ;_J_k,(c, C) (6.11) 96 _C_. = l- e-klt (6.12) S In this figure, the mass transfer is stronger at earlier times when the aqueous phase concentration of NAPL is lower, asymptotically approaching a normalized value of concentration of approximately 0.8 after about 12 hrs of residence time. Figure 6.10 illustrates how the residence time decreases for decreasing Da values (increasing velocities), resulting in a range of normalized effluent concentrations that decrease as the Da value decreases. In the lower values of Da, equilibrium solubility of NAPL is not achieved by the surfactant enhanced aqueous phase. This inefficiency is illustrated by the longer clean-up times (e. g., 1* E 88 for Da = 100, t* E 163 for Da = 1). As the trapped residual NAPL is removed from the soil, the increase in the effective aqueous phase porosity will result in a decrease in local flow velocity and subsequent increase in local residence time of the surfactant enhanced aqueous phase. The implicit transport model was used to evaluate the significance of this local change in interstitial velocity. In the first two studies, velocity was held constant and predicted based on either total porosity, n, n=-—"— (6.13) or the initial effective porosity, ne, V..-V.. n:— V t (6.14) where Vv is the volume in the voids or pore space, V" is the volume of trapped residual NAPL, and V, is the total volume of the soil and pores spaces. By predicting the velocity based on total porosity, the model assumes that the trapped residual NAPL does not influence the permeability of the soil. By predicting the velocity based on effective porosity, the model accounts for the reduced permeability the trapped residual NAPL In a third study, velocity was predicted at each time step within each element based on local 97 changes in the effective porosity as the residual NAPL volume is reduced due to surfactant dissolution. The results presented in Figure 6.11 suggest that the solution based on local changes in velocity differs significantly from the solution based on a constant velocity predicted by either total or effective porosity. As such, local changes in effective porosity will be incorporated into the code to predict local velocity and residence time. A numerical simulation was compared against actual data collected from the effluent end of a column flushed continuously with a 5% solution of the nonionic surfactant (Fig. 6.12). The model does not predict the trend in the experimental data at later time which can be explained in part by the limitations in the use of the lumped mass transfer coefficient. This coefficient is a function of both the specific interfacial area between the NAPL and the aqueous phase and a measure of the mass transfer across this interface. Not only is the actual internal contact between the aqueous phase and the NAPL difficult to quantify experimentally or mathematically due to the complex size and shapes of the ganglia, but the interfacial surface area changes with time as the NAPL dissolves into the aqueous phase (Wilson et al. 1989; Miller et al. 1990). Miller et al. (1990) and Powers et al. (1991) evaluate the mass transfer and the change in interfacial area as a function of measurable parameters of the soil and fluids. A second limitation of the model may exist if preferential flow paths or pore constrictions are present within the soil prior to or during treatment of the contaminated soil with surfactant. The model assumes a uniform distribution of trapped residual NAPL and a constant interstitial velocity within an element which does not account for the aforementioned conditions. However, the data compares more favorably to the implicit transport model than comparable data in a similar long term dissolution study evaluating an equilibrium model and a kinetic model developed by Priddle and MacQuarrie (1994). In their study, the lumped mass transfer term was also measured in a flow interruption study. 98 A higher value of Da (i.e. 100) directly translates into lower pumping rates but an increase in residence time when compared to a lower value of Da (i.e. 20) which translates into a higher pumping rate but less residence time (Fig. 6.13). However, both cases will result in 70-90 pore volumes of contaminated water based on the assumption that all of the enhanced aqueous phase is recovered and that it is not diluted by ambient groundwater. The validity of these assumptions will be addressed in the 2-D model study which evaluates the flow paths of the injected surfactant enhanced aqueous phase in the next section. The numerical result of the long term dissolution study of the column experiment was used to evaluate error propagation in the model. Assuming that the mass transfer coefficient, residual NAPL saturation and dispersivity are independent, simulations were modeled changing these values in different combinations to the average value plus the error associated with the variable. The values used in each simulation were obtained fi'om . Table 6.1 and shown in Table 6.3. The maximum relative error between the simulation with average values and the simulation with the values shown in Table 6.3 is recorded in the fourth column. The value of dispersivity was varied to include dispersivity in Ottawa sand with and without trapped residual NAPL, resulting in a 0.6% and 2% relative error respectively. This indicates that error in dispersivity does not have a strong influence on the model for the system under consideration. The largest error (94%) occurs when the error in the saturation of trapped residual NAPL is evaluated. It is important to note that this error occurred at later time, where the predicted values of NAPL concentrations are relatively small. When the error is propagated for all three terms, the maximum error is 10.3%. 6.5 Verification of 2-D Numerical Code The potential surfactant enhanced remediation of an unconfined aquifer with a region of trapped residual LNAPL contamination near the capillary fiinge was firrther 99 investigated using a United States Geological Survey (USGS) model for saturated and unsaturated flow and t_ra_nsport, SUTRA (Voss 1984). The simulation models a vertical cross section of an unconfined aquifer across the saturated and unsaturated zones (Fig. 6.14). The lower and upper boundaries are no flow boundaries whereas the side boundaries are constant head. The region below the water table is approximately 0.7 m wide, with a capillary fiinge approximately 0.2 m wide. The remaining upper region of the aquifer is the unsaturated vadose zone. The 0.8 m x 0.3 m contaminated region is near the center of the aquifer extending through the capillary fiinge and below the water table. These dimensions were chosen to simulate a physical lab scale model which is available to conduct supporting experiments. It should be noted that the prototype scale could easily be increased. The aquifer is divided into rectangular elements 0.1 m x 0.1 m except in the region near the capillary fringe. In this area, the aqueous phase saturation and relative permeability may change from saturated to near residual Saturation values within one or two element lengths. To account for this, the vertical increments are reduced to 0.02 m in this region. Element and node numbering are show in Figures 6.15-6.16. The pressure-saturation and relative permeability relationships in the vadose zone were initially estimated based on van Genuchten's equations (Chapter V). A pressure- saturation curve using these values is shown in Figure 6.17. A steady state flow field is generated for each well scheme. To verify the model, the location of the top boundary of the saturated zone was compared to an analytical - solution (Wang and Anderson 1982 ) using the Dupuit assumption of horizontal flow where: 1(5sz — =R 6.15 2 5x2 ( ) 100 In this equation, K is the hydraulic conductivity of the saturated soil, H is the hydraulic head, x is the length and R is the recharge rate which is zero for the solution being considered (Fig. 6.18). The general solution is: H2 =alx+a2 (6.16) where a 1 and a2 are constants determined by substituting the constant head boundary conditions at each reservoir. In the analysis, a 0.01 gradient was maintained between the reservoirs, varying the LHS head between 1-0.2 m in 0.2 m increments. Figure 6.19 shows the results of the comparison between the numerical code and the analytical solution where the relative error, e, was determined as: e: IHWM—HWWIJOO (6.17) H analytical The 0.1% error in the specified heads is the result of error in the code which only maintained accuracy to 5 significant figures. The largest error, approximately 0.27%, occurred at the smallest elevation of the reservoirs evaluated. These results verify the use of the flow model in SUTRA. The transport model was compared against an analytical solution for an instantaneous point source at the origin of an x-y coordinate system at time t = 0 in a saturated, homogeneous, isotropic medium (Fischer et al. 1979; Freeze and Cherry 1979). The initial condition can be expressed as: C(x,y,0)=M6x6y (6.18) where M is the mass of the contaminant introduced at the point source and 6x and By are the incremental thicknesses of the injection point. As the contaminant mass is transported by the flow through the porous media, the concentration of mass at time t is given by: 2 _ t 2 C: exp _(x v) — y (6.19) 47mb,/D,D, 40,1 419,1 101 where n is the porosity, b is the thickness of the aquifer and D, and Dy are the coefficients of dispersion in the x and y directions. The numerical code simulated the injection of an instantaneous point source by injecting 0.005 kg of contaminant mass at a center node of a saturated 1 m x 2 m aquifer in 10 seconds. Figure 6.20 shows the comparison of the analytical solution with the numerical code with contours based on the fraction of mass 10 minutes after the instantaneous injection of the solute mass. In the model simulation, the grid spacing was maintained at a constant value of 0.1 m. The simulation assumed negligible molecular dispersivity (D* = 0), longitudinal dispersivity of 0.1 m (01,) and transverse dispersivity (a ,) one-tenth the value of the longitudinal dispersivity. These values are within the range of values of dispersivity reported for sandy homogeneous soils measured in both the laboratory and the field (Freeze and Cherry 1979). Additional data and parameters used in SUTRA are summarized in Appendix D. The numerical transport code predicts the transport of the solute more accurately fiom the middle to the outer edge of the plume as indicated by the 1% and 3% mass fraction contour lines. At the injection point, as indicated by the 5% contour line, there is less agreement. However, the results indicate that the numerical code reasonably predicts solute transport as modeled by the analytical solution. Based on the results of the comparison of the flow and transport model used in SUTRA with the two analytical solutions, SUTRA was selected to further evaluate the use of surfactant enhanced remediation. 6.6 Two Dimensional Model Simulations The primary objective of applying hydraulic controls is to deliver surfactant into a contaminated region where the relative permeability is reduced, to ensure efficient contact time of the surfactant with the contaminated region, and to recover contaminant laden surfactant enhanced groundwater. The evaluation of well systems, designed by the 102 placement of wells and pumping rates, will be based on these considerations. The geometry of the system is illustrated in Figure 6.21. Dimensionless numbers, based on the dimensions of the contaminated region with respect to the aquifer domain will be used to indicate the placement of the wells. Prior to pumping, the flux rate per unit width through the contaminated region is Qa. Subsequent flux rates per unit width of the source and sink wells (Q,) are normalized by Qa- 7:9; 620 Q. Q, (- ) The distance to the source and sink wells in the x-direction fi'om the centerline of the contaminated region, d,, is normalized by the length of the contaminated plume, I. x; = -——'- (6.21) The distance to the source and sink wells in the y-direction from the upper boundary of the contaminated region, 6,, is normalized by the width of the contaminated plume, w. y;- =3 (6.22) w The dimensions of the contaminated region are compared in the aspect ratio w' where: w' = 1; (6.23) A summary of the well schemes evaluated in this research is presented in Table 6.4. In the case studies presented, the aspect ratio was maintained at a constant value of 0.375. An initial simulation study assessed the effects of the reduced permeability and reduced effective porosity resulting from trapped immobile phases at the capillary fringe on surfactant flow into the contaminated region. Soil and fluid characteristics were maintained to represent the conditions used in the previous 1-D study and experimental 103 work. In the contaminated region, the permeability was reduced to 0.5K and the effective porosity to 0.8211. A 6% surfactant solution was injected at a rate of 0.5 kg/s (0.5x10'3 m3/s) and monitored over time as it migrated between source and sink wells of equal strength (Case la; Table 6.4). The results were compared to a similar simulation conducted for a completely homogeneous aquifer (Case lb; Table 6.4). Figures 6.22- 6.23 compare the migration of the plume both cases, mapping the surfactant concentration contour plots from 0.01-0.05 (l%-5%) at t = 1.67 hr., 3.3 hrs. and 5 hrs.) The concentration contour plots were developed fi'om data generated by SUTRA and imported into Surfer which incorporated kriging (Golden Software; Golden, Colorado). The results indicate that the injection is slightly retarded in the study where the relative permeability and the effective porosity is reduced, but significant by-passing of the contaminated region does not occur. The results of the two simulations is further compared in Figure 6.24. In this figure, the 0.05 concentration contour (5%) is compared at 5 hrs. further supporting the conclusion that no significant by-passing is occurring. The contaminated region was subdivided into three subregions, each 0.1 m x 0.8 m, in order to fiirther evaluate the flow characteristics of the surfactant enhanced dissolution of the trapped residual NAPL. The upper region in the capillary fiinge is subregion 1, below the approximate location of the watertable is subregion 2, and the lower region is subregion 3. If flow through the subregions is horizontal, the 1-D transport model can then be used to predict clean-up in the subregion as a 1-D column. In such a case, the velocity of the region, incorporated in Da, can be directly used to estimate the time required for NAPL dissolution (Fig. 6.13). In Table 6.4, Ba in the three subregions is shown as Da(1), Da(2) and Da(3), respectively. Prior to pumping, estimates for flow variations in these 3 regions were made for the case where the relative permeability and effective porosity were reduced as well as for the homogeneous aquifer (Case 8-9; Table 6.4). The coefficient of variation (the standard deviation divided by the 104 average value) of the velocity within a region was estimated based on the magnitude of the velocity at the centroid of each element. The coefficient of variation is indicated for each subregion in Table 6.4 as CV(1), CV(2) and CV(3), respectively. In the heterogeneous case, the CV in subregions 2-3 is 0.06 compared to 0.003-0.002 in the homogeneous case, indicating a greater variability in the velocity for the heterogeneous region. In the region of the capillary fringe (subregion 1), the CV is much higher (0.32), indicating a significantly higher degree of variability in velocity. Above this region, the relative permeability of the aqueous phase is significantly reduced. As a result, the top of the capillary fiinge is similar to an impermeable boundary where streamlines converge. Velocity vector plots, generated by the supplemental program included with the SUTRA documentation (Souza 1979), further illustrated these differences in Figure 6.25-6.26. In these plots, the velocity vectors are scaled by the maximum velocity vector while indicating the direction and magnitude of the velocity. The smaller grid in the capillary fiinge results in a higher concentration of velocity vectors, but does not necessarily represent an increase in flow or velocity. The area of reduced relative permeability and effective porosity is shown by the shaded region in Figure 6.26, which is not included in the completely homogeneous aquifer studied in Figure 6.25. Figures 6.27-6.28 show the velocity vector field for Case la-b, where source and sink wells of equal strength are used to inject a surfactant. As shown in Table 6.4, Ba is reduced in the three regions, indicating an increase in the local flow velocity. Variations in the upper region are slightly increased from 0.32 to 0.34-0.35 (6-9%). The coefiicient of variation for the velocity in the middle region is significantly increased in the homogeneous case (1b) from 0.003 to 0.08 and fiom 0.002 to 0.08 in the lower region. In the heterogeneous evaluation (Case la), the increase in variability in the middle and lower regions is between 33-50% (change in the coefficient of variation = AC.V. = 0.02- 0.03 respectively). 105 Additional well schemes were evaluated (Table 6.4). Concentration profiles at t = 50 hr. were used to measure the effective zone of capture of the surfactant plume. In these studies, dispersivity and molecular diffusion were considered negligible using a value of 0.5 for the weighting parameter UP in SUTRA. This was done in order to monitor the sharpest concentration gradient, as suggested in the manual (Voss 1984. p. 10). The concentration contour graphs were evaluated by comparing the area captured by the 5% surfactant plume (A 5%), the total area of the contaminated region (A c), and the area of the contaminated region not captured within the 5% surfactant plume (Au). Two measures of the zone of capture were developed based on the ratios of these areas. Aso/ : -——° 6.24 51 Ac ( ) A 6‘ = 1- u 6.25 2 A ( ) 0 Values of 81 >1 suggests that the surfactant plume is migrating through uncontaminated regions of the aquifer in addition to the contaminated area targeted for treatment, where as 81 < 1 suggests that the surfactant plume cannot treat the entire contaminated region. This measure of the zone of capture does not evaluate the extent of the contaminated region left untreated by an injected 5% solution of surfactant, which is provided by the second measure, 82. This measure of the zone of capture provides an estimateof the area left untreated or else treated by a surfactant enhanced aqueous phase diluted by ambient groundwater such that the surfactant concentration is less than 5%, where dissolution of trapped regional NAPL may still occur. Figures 4.6-4.7 indicates a CMC < 1%, supporting that surfactant dissolution is not limited to regions of 5% concentration. Analysis based on the dissolution of NAPL and the rate limited mass transfer variations based on surfactant concentrations would require a more complex model and additional 106 experimental work beyond the objectives of this research. Despite these limits, this simplified analysis provides a valuable estimate of the evaluation of hydraulic control. In Case 2, screened injection and recovery wells of equal strength (Q; = Q; = 1.49) were placed below the water table and outside the predicted contaminated region. The resulting concentration contour plot and velocity vector plot are given in Figures 6.29-6.30. Based on the concentration contour plot, 81 = 1.73, as evident by the large 5% surfactant plume which extends below the contaminated region. The pumping scheme is highly efficient at capturing the contaminated region as evident by 82 = 0.99. For the pumping strategies studies, this scheme is the most efficient in capturing the contaminated region within the 5% plume. As state earlier, lower surfactant concentrations also enhanced the dissolution of the trapped residual NAPL in the contaminated region. The entire contaminated region in this study is captured by the surfactant plume < 1%. However, the recovery well may not be recovering all of the contaminated laden surfactant, and is definitely not recovering all of the surfactant. The velocity is relatively horizontal in the contaminated region as indicated by the velocity vector plot and variations of the magnitude of the velocity in the three subregions. Consistent with the previous considerations of velocity differences in these subregions, the upper region of the capillary fringe shows the highest variability, as indicated by the coefficient of variation (CV) in region 1 equal to 0.35, as indicated by CV(l) = 0.35. The CV in the other two regions is increased compared to Case 8 with no pumping. Because of the higher flow velocity due to pumping, Da is increased in all three subregions, compared to Case 8. The average velocity in each of the subregions of this study was used as input in the 1-D implicit transport code to predict the fraction of trapped residual NAPL remaining after flushing with 60 pore volumes of surfactant. The results (Fig. 6.31) indicate that the variation in velocity does not result in dramatic differences in clean-up time. 107 In Case 3 (Figures 6.32-6.33), the strength of the screened injection well was reduced 50% fi'om the previous study. As a result, the total area of the surfactant plume was reduced, as evident in el = 0.87, but less of the contaminated region is captured in the 5% surfactant plume as indicated by 82 = 0.95. The CV in the upper region increased, but slightly decreased in the lower two regions. The Da increased due to the reduced strength of the injection well compared to Case 2. The velocity vector plot indicates that the flow is relatively horizontal, indicating that the 1-D transport code may be used to predict NAPL removal. The graph of the surfactant concentration profiles further indicates that all of the contaminant laden surfactant and all of the injected surfactant is removed from the groundwater environment by the recovery well. In CaSe 4 (Figures 6.34-6.35), the strength of the screened injection and recovery wells were equal (Q; = Q; = 1.49) but placed within the contaminated region. In this study, 81 = 0.91. However the inefficiency of the scheme is evident in so far as 82 decreased dramatically to 0.83. Of the cases studies, this pumping scheme captured less of the contaminated region than any other. The recovery well does not recover surfactant which may have flowed through the contaminated region, thereby spreading NAPL contamination into previously uncontaminated regions of the aquifer. In addition, the velocity vector plot indicates that the velocity field in the contaminated region is unidirectional and non-horizontal, negating the use of the 1-D model as a tool to firrther evaluate this pumping scheme. In Case 5 (Figures 636637), a smaller screen well is evaluated just below the watertable but outside the contaminated plume (Q; = Q; =1.49) in an attempt to deliver less surfactant below the contaminated region. As a result, more of the contaminated region was captured (82 = 0.97) but the size surfactant plume increased (81 = 1.47). The velocity vector plot indicates that the velocity is relatively horizontal in the contaminated region, but the concentration contours indicate that the surfactant is not completely captured by the recovery well. 108 The lowest injection and recovery well strength was evaluated in Case 6 where Q; = Q; = 0.3 (Figs. 6.38-6.39). At this low flux rate, the surfactant was slowly injected into the groundwater system. As a result, the 5% surfactant plume is diluted by ambient groundwater. The velocity vector plot suggests that a small degree of by-passing may occur, as indicated by the velocity vectors outside the lower left side of the contaminated region. The zone of capture is extremely small compared to the other situations studied and was not evaluated in this case. Case 7 (Figures 6.40-6.41) evaluated a pumping scheme where the surfactant was injected between injection and recovery wells of equal strength outside of the contaminated region at a flux which maintained flow through the contaminated region slightly above the flow that would be in the region without pumping (Q; = Q; = 1.19). As illustrated in Figure 6.40, the 5% surfactant plume captures most of the contaminated region, but extends over a larger region. In addition, the injected surfactant is not captured by the recovery wells, as suggested by the concentration contour plot and the velocity vector plot . In all of the cases studied, additional evaluation based on the coefficient of variation of the velocity in the subregions is summarized in Table 6.4. This table also summarizes the results of the zone of capture measurements. Comparisons of this table with the concentration contour plots and velocity vector plots indicate that the most efficient pumping scheme is Case 3, where screened injection and recovery wells are placed outside the contaminated region, but pumped at unequal strengths such that Q,’ = 0.5Q, = 0.75. 6 .7 Summary A 1-D implicit transport model was developed and used to evaluate the use of a surfactant enhanced aqueous phase to promote the dissolution of trapped residual NAPL in conjunction with 2-D modeling using the USGS saturated-unsaturated transport model 109 SUTRA. The primary focus of the research was to evaluate the use of hydraulic controls to emciently use surfactants to enhanced the dissolution of trapped residual LNAPL near the capillary fiinge. The study was conducted in a homogeneous unconfined sandy aquifer with a region of trapped residual LNAPL contamination near the capillary fringe. The vertical cross section of the aquifer extended 1m x 2m with a 0.8 m x 0.3 m contaminated region. These dimensions were selected based on an existing physical laboratory scale model, but the prototype scale could easily be extended. Several different well schemes based on well location and pumping rates were compared- Surfactant concentration profiles and velocity vector field provided the basis for selecting a pumping strategy based on 1) delivering the surfactant to a contaminated region; 2) ensuring sufficient residence time between the surfactant enhanced aqueous phase and the contaminant to minimize the cost of the surfactant and the amount of wastewater to be treated; and 3) recovering the contaminant laden surfactant enhanced groundwater. For the small aquifer studied, a surfactant enhanced aqueous phase flowing at local flow velocities will not reach solubility concentration of LNAPL after migrating through the contaminated aquifer. If the local ‘flow velocities are increased due to pumping, the dissolution of LNAPL into the surfactant enhanced aqueous phase may be further decreased. As a result, the primary use of the hydraulic controls were to promote the delivery of the surfactant into the contaminated region and the recovery of contaminant laden surfactant enhanced groundwater. The strength of the wells and the location of the well with respect to the dimensions and location of the contaminated region are summarized in nondimensional numbers in Table 6.4. The results indicate that the most eflicient design maintained a constant injection rate below the rate of the recovery well set outside of the contaminated region. The results support the need for further research in the use of surfactant enhanced groundwater remediation of trapped residual NAPL, including addressing different aquifer soils or dimensions. 110 In less permeable soil, slower velocities may result in a more optimum use of the residence time through the contaminated region. The surfactant may also be more efficient when evaluating a larger contaminated region. In both cases, the maximum solubility may be achieved prior to recovering the contaminant laden surfactant enhanced ground water. In these situations, the flow may need to be increased to optimize the cost. Further evaluation of the capture zone would also need to be conducted. In this study, heterogeneity was limited to the inclusion of a contaminated region where the relative permeability of the soil is decreased to 0.3 to 0.7 times Ksat due to trapped residual NAPL. In the field, heterogeneities are also present due to silt and clay strata that may reduce the permeability by a factor of 1000 to 10 million (Mackay and Cherry 1989). If the site investigation to determine the aquifer soil characteristics was limited due to economic constraints or limitation from existing structures (e. g., buildings), such strata may not be factored into the evaluation of the hydraulic controls. Based on these considerations, further evaluation should also incorporate changes in the efficiency of the hydraulic controls which may occur due to undetected lenses of clay or silt . 111 ‘19 " —0— ANALYTICAL sour. 03 -. <> mmcrr sour. 0 0.1 0.2 0.3 0.4 0. 5 0.6 0.7 0.8 0.9 l X/L Figure 6.1. Implicit numerical solution compared to analytical solution ( Cr =0.5; L =15 cm; a) = 0.5; Ba =1; Ax = 0.5 cm) "r o 1. 0 o o 5‘ o o A 35" E o “' o o is 0 'Maximum °Minimum 2.! 1 0 0L t 1‘ H , . 0 10 20 30 40 50 60 70 80 90 100 DI Figure 6.2. Maximum and minimum relative error over a range of velocities as indicated by the range of Da (Cr = 0.3; L = 15 cm; a) = 0.6; Ax = 1 cm). 112 100 10 A a" v a —v—Cr-o.3 a +Cr-05 “’ 1 +Cr-0.7 01 I *7 1 I I ‘ I f T fi 04 05 06 0.7 08 0.9 10 (D Figure 6.3. Summary of study to optimize the Courant number over a range of to values (L = 15 cm; Ax = 1 cm). 100 a : A A 9 MAX ERROR (v=l cm/min) o\' E 10 0 MIN ERROR (v=l crn/min) E A MAX ERROR (v=0.1 cm/min) . 8 E 1 A mm ERROR (v=0.1 cm/min) a j a a O. 1 > o 0.01 i i i i i 0.01 0.1 1 10 100 1000 DAMKOHLER NUMBER Figure 6.4. Relative error over a range of Da numbers represented in previous table (Cr = 0.3; a) = 0.6; Q = 0.5 mein; L = 15 cm; Ax = 1 cm). 113 1000 OMAXERROR(v-O.lemlrnin) o MINERROR (F01 mm) 3 100 a a a AMAXERROR(v-lanlmin) 3.4 AMINERRon-ran/tnni) ‘ O O a 10 A a H . 8 E 1 5 O a o o o o o 0.1 ‘ A A A A 001 t t i a i i i i 0.01 0.1 l 10 100 1000 10000 100000 Pe Figure 6. 5. Relative error over a range of Pa numbers (Cr = 0.3; a) = 0.6; Q = 0.5 mein; L = 15 cm; Ax = 1 cm). 1 ‘ .—---———'—“'—-—__.._...:-T-T7-T="—" ............ h" ............... 0,9 dr- ,// “....M'Wl ----- 1,.r"" .1", ------ 0.8 -U- ’3'.” l/,’ 31"" 0.7 a. [I l.‘ / 'I 0.6 ~- - — — — t‘ = 2 s 0.5 . 1' ," --------------- t. = z) 3 0'4 1.. '1' // ------- t. = w 0-3 " 2’ - ---------- t“ = 60 0'2 ._ ",1 0.1 ~- 0 ~ *fi t 4' i 41- i ----- + ----- - i i a ---i 0 0 1 0 2 0 3 0 4 0.5 0 6 0 7 0 8 0 9 1 X/L Figure 6.6. Fraction of trapped residual NAPL remaining in pores spaces over the length of the column over time (Da = 10; Cr = 0.3; a) = 0.6; L = 15 cm; Ax = 1 cm). 114 a 1‘-——-—-—~*"*————————“——~——‘—‘f - 0.8 - """""""""""""" g - _____ - - ~, ...... 30‘“ ”..-!” ...... I” _____ g ---------------- .4 0.6" ” ,,,,, , ..... I” --------- t‘-2 Q 0.5 .. f, ..... , "’ .................... ,.=,, z 0.4 + " ‘8 0.3 .. -------- t‘=40 .s ,2 . g . _ .............. 9:60 i. 0.1 -- k‘ 0 t t t . % o 0.2 0.4 0.6 0.8 1 X/L Figure 6.7. Dimensionless analysis of surfactant enhanced dissolution of trapped residual dodecane (Da = 1; Cr = 0.3; 0) = 0.6; L = 15 cm; Ax = 1 cm). .................... tfi=20 - --------- t"=40 L v [ :3: I" I - """""""""" t. = 60 FractionofNAPLRemaining PPPPPPPPP Ou—Nwhuc\~IOOVOI-' 0.2 0.4 0.6 0.8 1 X/L O Figure 6.8. Dimensionless analysis of surfactant enhanced dissolution of trapped residual dodecane (Da = 100; Cr = 0.3; co = 0.6; L = 15 cm; Ax = 1 cm). 115 1.0- 0.8 - 0.6 -4 C/c, 0.4-J 0.2-r 0.0 . 1 I T I V l 1 I V T T I 8 1o 12 14 16 18 time (hrs) @- Oj-I Figure 6.9. Rate-limited dissolution of NAPL into surfactant enhanced aqueous phase. 1 -r - -------------- Da=100 —————— Da=10 08 ‘ :7::T:::":“':‘:':”\‘ """" § ‘ - . ‘\. - --------- Da=4 Q A A A A A \,\ \ \ “ A ‘\ A ‘\ A Da=2 g 06 i an; E o o O o <> <> <> 0 0‘60 o O Da=1 H E\\\.‘!A O 30» ‘=.\‘x. A O o i 0 E g 1 ‘.‘ A 0 e '= l, x z . E x A O 0.2 r l, \‘ <> l “ A '=. ‘. 0 0 t + f t f 1 t #13 t w . 0 20 40 . 60 80 100 120 140 160 180 ti Figure 6.10. Normalized effluent concentrations over a range of Da. 116 1 “ OTOTALPOROSITY [-1 0.9 Z A EFFECTIVE POROSITY a 0.8 p g 0 7 O VARIABLE POROSITY E = ‘ H E 0. G g E 3.4 0 ’ A A A . O z 0.6 A A 8 0.3 i' O . A A «)- 0 . g 0.2 o . A A 0.1 ”J“ O O A 0 . fee a . 0 50 100 150 200 Figure 6.11. Comparing effluent concentrations when velocity is determined from total porosity, effective porosity and variable effective porosity. p—s J. .° xo X DATA .9 co ------------------ IMPLICU‘ CODE C Q X X X X °.°.°.°.. ~63th X NORMALIZED EFFLUENT CONCENTRATION . o o o at 05 X x X x X x Xx x x X X 50 100 150 t t O Figure 6.12. Experimental and implicit modeled effluent concentrations of dodecane in a 5% nonionic surfactant enhanced aqueous phase. 117 m-r Figure 6.13. Pores volumes needed to reach MCL over a range of Damkiihler numbers. 118 £39.. aoumsua $.82 .36 9.53 x% the AWGNDOH (IVEIH .INVLSNOC) - W i so >MM mo. i E 0.10” B o m > I. I f“ .‘ . .' 0.05 * 5. j .7 o.oo* ~ 00 05 1D 15 20 x-direction (m) Figure 6.19. Results of the comparison of SUTRA with analytical solution for determining the surface of the watertable through the aquifer. l.“ 0.8 1- O.“ '- 0.“ - Y-DIRBCI'ION (In) 0.20 I- ....... 0.“ l L l l I l I l l 0.“ 0.20 O.“ a.” 0.” 1.” 1.” 1.“ 1.“ 1.” 2.” X-DTRFCTION (m) Figure 6.20. Comparison of numerical and analytical solution for transport of an instantanteous point source. 123 C I i c source 5 H ............. .1. ................................................. u sink well ‘ well N d 1 ... d 2 Figure 6.21. Geometry used in evaluation of well placement. 124 0.20 '- T- 1.671! 1"0'0'1 1 1 1 1 1 1 1 0.. 0.. O.” 0.“ O.“ 0.“ I.” 1.2. 1.4 hfl 1.“ 2.“ .ea" _ r-xrw ,. ii-MI. . . . . . '. 1 ‘0. O.“ O.“ O.“ O.“ '0“ 1.” 1.“ 1.“ 1.“ 2.“ T-51br ..g l i-o.OI_L L l l l I l I a” 0.” ... 0.“ .0“ '0“ 1.20 1|“ 1.“ 1.“ 2.00 Figure 6.22 Concentration profiles as plume migrates through a region of contamination where the relative permeability and effective porosity are reduced due to trapped residual NAPL (Case 1a) at t = 1.67 hr., 3.4 hr. and 5 hr. 125 SOURCE NNK ............................................................................ T-L7M ll'0.01 l I l l l L l l O.” . O.“ 0.8 0.“ 0.60 0.9 1.“ 1.3 1.40 1.00 l.“ 2.“ 0.8 r T-13M O.” 1 i=0“ 1 1 L 1 4 1 1 1 0.. 0.20 0.“ 0.“ 0.“ ‘0“ ‘0” 1.“ 1.“ ’0“ 2.00 " 'edu3oe-a-u---.a--\vu-nn ....ln. ..................... 0.8 - T-Shr 1-0.01 .. l I ‘0. 0o” .0“ 0.“ 0.“ 1.“ 1.20 ‘0“ 1.“ ‘0“ 2.“ 1 1 1 1 1 1 1 Figure 6.23. Concentration profiles as plume migrates through a homogeneous medium (Case 1b) at t = 1.67 hr., 3.4 hr. and 5 hr. 126 A: 8.5 E... a“ 8:0 .3.— Eseg m «a 2:9:— =e3ah=3=8 new so b.2555 .vue 9..—arm 8.0 8; 0o.— 0v.— ON; 8.? 00.0 00.0 0V0 0N0 00.0 8.6 _ n _ . a _ _ _ 8612 Emuh . > . . w .1 8.6 3 one 208mm €255.28 H . M /. 19.6 3. one 2282 BomZmeonm . , , O .1 00.0 ....................................................................................................................................................... .. . . M. ............................................................................................................................................ 1‘4... 1..........................I........-t......t..ilth_ 8 .0 225 127 Ave 225 a 6:0 no. a... .862 £8; one 2:3... c5 zofiommak 2 A: 3 I S S 2 ed w to 3 ed A. A .H A A A A. .. 0 od Al Al Al al Al Al Al al Al Al ..Art Al Al Al Al A1 Al Al A1 Al Al. Al Al Al Al Al Al Al Al Al hA.I Al al Al. Al. Al. All Al. A1. All Al: Al Al Al Al Al Al Al Al A.I Al Al al A1 A1 A1 A1 A11 a1. A1 ..A All Al 41 41 a1 A1 Al Al Al Al ”A1 A11 A1 A1 A1. A1. A1 A1... “A1... A1 1% All 61 A, 41 41 Al Al Al Al Al 1 a1 Al Al- 51 A11 A1... A11 “A11 A11 m ..... .5 . .. 1 e o m h . .. _ A .. A H . m ) ... -.. 11-.....” ...... T ..r T “T T “T .l “T T ”1 .II ..II All H .. RV m A4, 4.! , a1 41 .Al Al .Al Al “.1 A1 “A1 A1 Ha... .1 “Mill M“ A n“ m . Al a! A 41 Al Al Al “Al Al ”Al A... .1 Al .61. a... a e\ e\ . >\ I..\ f II of . 0| 0| 5| 0| 0| 6| . 0| 0| H 01- Ol. H 61.. .1 H .1 b\ H \ ......u......a.........I.......1....».0.. ...... .....1........t......4......n...... ........ .....‘1, ....... . 1..-..............n...-.................r..........a:.‘1..........................1.a.....3................IJ"......H...1.3.33...........O!............a.....l....... ..... . ......t..o......‘............ .....hb ”6° . a o o a o o o . e I I a I O . 0 v . I I C I A: A...» use a 3.6 .e s... .392 3.8.0.» .3.» 9...»...— Aev zoiomfiak . 2 o; wd wd to No ad 128 d . . _ _ _ d d. ._ co Al Al Al ”Al Al. Al Al- XI AI HAl Al HAl. Au| 5| Al Al Al. Al Al Al Al .Al Al HAI All Al Al. led .0 fl Al Al Al» AI A... A1\ All Al Al Al All Al Al 4! AI A.| A1l A\u Al. N _. _ O T All A.‘ Al Al A\ 01 .1: 4| 0... .1 4| 0.1 t... 4' AI A|.. A\ A‘ A|I l _ ..od I _. O 4/ Al Al Al Al 08 ...: 0! 0| «I AI. AI. t... A11 *I. A‘ A\ F\ x N . _ \/ fl .7 r .1 r H ..H H H n ..H n M ..H ..n ..H ..n .\ m f A, II A, ll C! b... t3 08 53 £1 9... A‘ 5‘ A‘ L‘ b\ F\ ( . x , r r r - - .. - - .. , x x x x x m a. . J .. .. .. . . . L 129 A...» 03.5 fl 8.6 .e 8... .82: E83» .2.» 2:5 ON ”A 04 *4 NA CA wd 0.0 Yo Nd Cd _ _ _ . _ _ ~ _. ._ co 0 o A. A. W A. A. A: A: A: A: A: A. A. A. A. n A. A. A. A. A. o A A. A. A. Al Al Al N A: A: A: A. f A. A. A. 4 A. n 1 No 0 Q A. O. 0‘ L\ Al At Al H Al Al A! A! 4: A. I. a. A. O A A A A. R A\ A\ A. Al Al Al A: A: 4: f i o o o .. v.0 Q Q | \ ‘ ’ l O O O O O I 2 $ t O O. . , o 1 ed A. w A . s k . . 9 fl A r . a 1D I A K A A I l u u . m m u u u u u . . . K A A A A . , , , ,, . . . . . we o.— 130 " "§&¢ ‘ : —>—>_ —)->§ 1.0 0.6 _ 0.2 - 0.0 2.0 1.8 1.6 1.4 1.2 1.0 0.8 0.6 0.4 0.2 0.0 Figure 6.28. Velocity vector plot for Case lb (Table 6.4). 131 A...» 0335 N 8.5 .8.— »o... 38:3 gash—.350 5".» 95w... ®m._. 00; 0?; ON; 00.? om.o 00.0 OV.® 0N.® 00.0 . _ _ _ _ _ _. _ H . _ ooo , Sol. 28".» Al> l ON.® l 0V.® .1 00.0 W I 00.0 132 .992)? . . u I I 11“... 0 . . 9 1.0 0.4 0.2 0.0 2.0 1.8 1.6 1.4 1.2 1.0 0.8 0.6 0.4 0.2 0.0 Figure 6.30. Velocity vector plot for Case 2 (Table 6.4) 133 1.0” . Region 1 . ,5 Reglon 2 ’g 0'8 """"" Region 3 g b a: —l 0.6“ a... <2 . E O 0.4“ r: 0 . é a. 0.2- o 1 l J (2)0 O 2 0.4 . 0 6 0 8 1 0 X/L Figure 6.31. Fraction of mass removed in each region after surfactant flushing 60 pore volumes. 134 ®®.N Av.» 03': m 8.5 .5.— 3E ...—3:3 notabaougu .3.» 2...»...— Om; 00.w 0V; ON; 00... 0V.® ON.® 00.0 _ _ _ L _ . . _ 00.0 ,Sonm. affine An|> .l GN.® l OV.® I 00.9 KIV .... 00.0 135 A...» 03.5 ... 8.6 .8 3... 58> £8...» .9...» ea»...— cN wfi m: v— N_ c; we we to N6 o.o _ . _ _ .u a _ fl _ 9.0 o A. A. A. A. A. A. Al Al Al Al Al Al Al A. H A. A. . A. A. A. O. o. A. A. Al Al Al Al Al Al Al Al Al A. AI A. AI A» . _ ............. ... N.o O A. A. b. A. A\ A. A. Al Al Al Al Al Al Al Al A. A. A. 9 A A. . R N 4. A. A. A. A. o . . e R g A A. A. A. , o .o - ».c A. .v T t A. 5. Al 14% $ M; 5 Q ‘ . n . m w m a - n .m d . . u n .. u w . . . we A: 136 ®®.N .AV. o 2%: v 030 5m SE 58:8 8255080 .3.» oswfi 00:. 00;. 0?. ON; 00. 0m.® 00.0 OV.O ON.® 00.0 . _ _ _ _ _ _ _ L . q 000 . . Sol . Eomne > I ON.® ,l OV.® ,l 00-0 W l 0m.® .c.» 2......» e 3.6 .8 8... .3»: £83» .mn.» 25.: ON ”A o ~ v — N _ 9— w o w o to Nd od _ _ — q _ _ n _ _ CO e. f A. A1 Al Al Al Al Al Al Al Al Al Al 4. A. A. a. A. O. 0. a. A. A1 Al Al Al Al Al Al Al Al AI 4. A. l. t. t. - Nd A. A. A. A. A. A. A\ Al Al Al A! A. A. A. A. A. A. A. A. A. A. A. A. A1 A1 A\ Al Al Al A! A! A: 4. A. A. A. A. A. "M , l v.0 l A. A. O. 0. D. 1 f 9 A. A. O. A. A. O. | l n i A. O. O. l. .. v.0 ‘I ' ’ I O O ‘ .A * MM A. o A . . . A A R .. n u u U u u H u o .M a r A A A . v A A n . ...... : . . ... ..1... .. ”o o.— 138 Av.» asst m 02.0 ..8 .2.— .=_S=3 5322850 .3.» PEEK 0N6 om; QO. 0?. GN; 00.? 00.0 00.0 0V.® 00.0 _ _ _ _ _ _ A . _ 00.0 wool Homna +|> I ®N.® I OV.® I 00.0 V 8.0 139 Ava 235 m 3.5 .3.— 3... .580.» £85» .5.» 2:5 QN «A w; VA NA CA ad v.0 to N6 od _ _ _ _ a A ~ u 0.6 1 N6 I to . . . . A K n . . 1 0.0 O ' I I ‘ I . .m . . . m , V . n. n H N. M. W n .u , J . , m6 A: 140 ®®.N .93 3.3.5 e 85 ..8 «a... 53:8 53955950 .wmé charm E 225202 ®m.— ®0.F ®V._ ®N.F ®®.F ®mu® ®O.® ®V.® ®N.® ®®.® . A A _ _ _ q _ . _ 09 ® . W W :21 .2 0m NH A > _ _ - 8.9 ‘1 0V.® ®0.® ®m.® ®®.F (w) Momma-A 141 Av.» 0535 e 030 he .2.— ..83> .0323; in.» 9..-Eh QN w.— A: v; A: ad ed v.0 Nd ed ,. .. . .— A A A. A o o A. A. A. A. A. A. A. . A. A. A. H A. A. _ A. A. A. A. A. A. A. A. A. A. Al A. A. , A. A. A. A. A. - No A. A. A. A. A. A. A. A. A. A. A. A. A. A. A. A. A. A. A. A. A. Al A. A. A. A. A. A. A. A. . - v.0 Al Al A. A. A. A\ A. A. A. A. Al Al A. A. A. A\ A. A. A. A. o - 9o 4.. AP A. A. A. A! A A. A. A. I 4! 4r 4. A. 04. R A. A. A. i n u n u n u n n n t f l I. ! I. \ Q t. K . .. ._ J . ... . ., .. .. .. .. mo o.— 142 Avd as“: b 980 .Su SE ...—3:8 grab—.850 .36 PEME as 22523“ ®®.N 0m... 00; ®v._ ON; 00.? 0m..® 00.0 OV.® ®N.® ®®.® _ _ _ _ ._ _ _ _ _ ®®.® 0N6 ®V.® ®o.® ®m.® ®®._ (w) NOILD'ERIICI'A 143 Av.» ...—act b 930 .8.— «o... .883 hag—Q, .3.» 8%.: ON «A m: o; «.0 o 0 v6 Nd od .. .. . 1 . . 3 A. A. m A. A. H A. A. Al Al Al A. A. A. A. w A. A. A. A. ”A. AI A. A| Al Al Al Al A. A. A. V A. A. . ................. .. . : : ........ .I Nd A. A. WA. A. MA. A. Al Al A. A! A. A. A. A. A. A. A. WA. A. .A. A\ Al A! Al Al AI 4. A. A. A. Al Al A. A. A\ N f A. A. 0 AI 4. A. A. I N A 0 O A. U o ..... l 0.0 Al 41 WA. A. 2 fl A A A. W . . A. A. A. f of A A 4M 4r 4. f 4r fl A A ¢ Ar Ar 4, 4r fl 1 I v A. A. 4' u u “ . A .. . ._ .. .. .. .. .. mo A: 144 Variable Value Source dispersivity, a 0.061 cm Pennel et al. 1993 dispersivity, a (with 0.136 :t 0.021 cm Pennel et al. 1993 trapped residual NAPL) . Sm 0.179 :t 0.004 measured density NAPL, p" 0.748 i 0.003 g/cm3 measured equilibrium solubility of 2005 j: 40 ppm measured (batch NAPL in 5% surfactant, experiment) CS lumped mass transfer coefficient, k, 0.387 a: 0.047 hr -1 measured (flow interruption study) porosity, n 0.38 i 0.013 measured Table 6.1. Soil and fluid properties used in model simulations. Contaminant k, (hr '1) Reference Naphthalene 0.081 Priddle and MacQuarrie 1994 Acenaphthenc 0.055 " Flourene 0.074 " Phenanthree + anthracene 0.079 " Benzene 0.0001 Borden and Kao 1992 Tolunc 0.0004 " Xylene 0.0004 " Aliphatic hydrocarbon 0.0004 " Table 6.2. Representative range of mass transfer coefficients (k1). 145 k, (hr ‘1) Sm on (em) Maximum relative error (%) 0.434 0.179 0.136 28% 0.387 0.183 0.136 94% 0.387 0.179 0.157 0.6% 0.387 0.179 0.061 2% 0.434 0.183 0.157 10.3% Table 6.3. Error propagation for the lumped mass transfer coefficient (k1), saturation of trapped residual NAPL (Sn). and dispersivity (a). 146 ...—95:3 8.3.6.3 he eases—«>0 o... .8.— 8Eog3 =9: ..e baa—Eam 6.» 03:. :03 Bag :8 on he.“ 59% omega . 290mm 98.58.4528; Bod Eagamgm oz .. $529. maomzmoozom E Bod Eagéazbm oz ... <2 <2 83 83 N3 2.. ...2 on; ... a <2 <2 83 83 N3 9: 35 :3 .. a 33 :4 :3 23 m3 32 92 on; a: ...: .3 .3 «2 n3 5 games... 2:33 So 83 N3 :.._ 33 33 33 33 .3 .3 n2 n3 3 :3 t; :3 m3 .3 a; 1.. «S a; 3: m3 m3 n2 «S n 33 33 :3 33 23 33 «3 33 a; a; .3 .3 33 n3 3 n3 :3 23 23 e3 :3 R; s; a: n3 .3 .3 24 2.. m 23 MS :3 :3 W3 32 n2 «2 a; a; .3 .3 n2 ...? N <2 $2 $3 83 .3 33 83 84 a; a; $3 83 n2 34 a <2 <2 :3 23 m3 ”2 o: 32 a; a; $3 $3 24 n2 2 No x. 8% «So «So 35 $5 3 5 "m G ..a ”a ..a w ”.65 Chapter 7 Dissertation Summary and Recommendations 7 .1 Summary The large number of sites identified for remediation by the United States Environmental Protection Agency supports the need for engineering solutions to confine damage, protect drinking water and to decontaminate aquifers. These sites vary widely in the geological characteristics and types of contaminants present, placing further demands on the technologies developed. This research presents a feasibility study of the hydraulic measures which influence the flow pattern and the resulting removal of a nonaqueous phase source of contamination within the porous matrix. Although focused on the use of chemically enhanced dissolution of trapped residual LNAPL at the capillary fi'inge, problems of in-situ delivery and recovery of treatment is common to other remediation techniques. The design parameters evaluated were the number of wells, the location of the well, and the pumping rates. The primary objectives of the use of hydraulic controls were to: 1) deliver surfactant into the contaminated region; 2) ensure sufficient contact time of the surfactant with the contaminated region; and 3) to recover contaminant laden surfactant enhanced ground water. A The initial three chapters of this dissertation present an introduction to the research, a literature review and an overview of the materials and methods used in the experimental work. The latter three chapters contain the results of experimental and numerical studies to promote surfactant enhanced dissolution of trapped residual NAPL at the capillary fringe. Each phase of the research has been presented in a separate 147 148 chapter that can stand alone, with a general summary presented here. The reader interested in more detailed summaries of individual phases of the work is directed to the summary section at the end of each chapter. The first experimental phase of the dissertation is presented in Chapter 4. The specific goals included: 1) developing an analytical technique to . measure the concentration of dodecane in a surfactant enhanced aqueous phase using head space gas chromatography; 2) comparing the enhanced solubility of NAPL measured in batch experiments with that observed when the NAPL is trapped as a residual in a porous media; and 3) investigating the non-equilibrium effects of surfactant enhanced solubility of trapped residual NAPL. The use of surfactants caused heavy sudsing and the formation of an emulsion during both liquid-liquid extraction and solid-liquid extraction procedures. As a result, an analytical method was developed using head space gas chromatography using a Perkin Elmer PE Autosystem gas chromatograph equipped with a flame ionizer detector and a PEHS40 automatic headspace sampler. The use of gas chromatography to measure the concentration of NAPL in surfactant was shown to be dependent upon the partitioning of the NAPL from the aqueous phase into the gaseous phase. Tests show that the degree of partitioning is strongly influenced by surfactant concentration in the aqueous phase. To overcome the effect of surfactant concentration, samples are diluted 100:1 in 5% surfactant. The detection limit for the gas chromatography is approximately 10 ppm. Batch experiments showed that a 5% solution of Witconol NP-l 50 enhances the aqueous phase solubility or dodecane fiom 0.035 ppm to approximately 2000 ppm. In the porous matrix, the solubility is enhanced to approximately 1600 ppm, due in part to the reduced contact area available when NAPL is trapped as a ganglia compared to the complete mixing in batch systems. Flow interruption studies were used to measure the lumped mass transfer . coeflicient of dodecane into a 5% solution of Witconol NP-150 149 which concluded that the dissolution of dodecane into the surfactant is a rate-limited process, but not prohibitively slow. Chapter 5 presents the second experimental phase of the study. Column studies were conducted to develop a better understanding of the relative aqueous phase permeability in the region near the capillary fiinge. Previous measurements by petroleum engineers of the relative permeability-saturation relationship of the aqueous phase beyond the regions where both phases are continuous have been limited to studies in sandstone and glass beads. This research considered that relationship over a range of trapped residual immobile phase saturations in a natural unconsolidated soil. As with the previous research by petroleum engineers, these experiments required a separate column experiment for each data point. The maximum aqueous phase saturation was reduced to approximately 85-89% due to the trapped residual nonwetting phase, reducing the relative permeability of the aqueous phase to 0.55k, - O.8k,.. A separate experiment was conducted using a single column in a long term study of the enhanced dissolution of trapped residual NAPL to provide a continuous measurement in this region. The results show that the continual increase in the aqueous phase saturation and relative permeability follows the trend of the previous experiment. The combined results of these two experiments provide a detailed image of the relationship of the relative permeability and saturation of the aqueous phase in this region. A third set of experiments was also conducted that measured the relative permeability of the aqueous phase in soil columns where both a trapped residual NAPL and a trapped residual air phase were present. The results show that the two trapped residual phases reduce the saturation of the aqueous phase to approximately 50% - 85%, which is a larger range that with a single phase trapped. However, the aqueous phase permeability remains at a relatively constant value of approximately 0.351., compared to the larger range when only one phase is trapped as a residual. Fitting parameters derived from curve fitting pressure-saturation curves in research conducted by Soeryantono et al. (1994) and Powers et al. (1992) were utilized 150 to evaluate the use of Corey's and van Genuchten's equations for the permeability- saturation relationship in the region where the aqueous phase permeability is increased as the trapped residual nonwetting fluid is decreased. The results indicate that the fitting parameters do not adequately predict the relationship in this" region of interest. Therefore, the raw data may need to be used directly in design and modeling. An implicit l-D transport code was developed in Chapter 6 to predict the removal of trapped residual NAPL using the lumped mass transfer coefficient measured in Chapter 4. Results were presented using dimensionless parameters which represent velocity, length, mass transfer and dispersion. In cases where horizontal flow may be assumed in an aquifer, the model is usefirl in optimizing the pumping rate when considering the number of pore volumes of surfactant required for treatment, the amount of waste water generated and the residence time required to promote near equilibrium saturation of dodecane into a surfactant enhanced aqueous phase. A numerical simulation was compared against actual data collected from the effluent end of a column flushed continuously with surfactant. The model did not predict the trend in the experimental data at later time which can be explained in part by the limitations in the use of the lumped mass transfer coefficient. This coefficient is a fimction of both the specific interfacial area between the NAPL and the aqueous phase and a measure of the resistance to mass transfer across this interface. Not only is the actual internal contact between the aqueous phase and the NAPL difficult to quantify experimentally or mathematically due to the complex size and shapes of the ganglia, but the interfacial surface area changes with time as the NAPL dissolves into the aqueous phase. A second limitation of the model may exist if preferential flow paths or pore constrictions are present within the soil prior to or during treatment of the contaminated soil with surfactant. This in part also explains why the enhanced solubility of NAPL is reduced in the porous matrix compared to the enhanced solubility achieved in batch experiments. 151 An existing USGS flow and transport model for unsaturated-saturated flow was used to evaluate the hydraulic controls a 2-D laboratory scale model aquifer in Chapter 6. Pumping rates, the number of wells, and the location of wells were evaluated using SUTRA in addition to the 1-D implicit transport model which evaluated the residence or contact time directly. Delivery of the surfactant enhanced aqueous phase and the recovery of the contaminated fluid was determined from velocity vector plots and surfactant concentration contour plots which predicted the flow paths resulting from the hydraulic controls. The study Was limited to a 2 m x 1 m vertical cross section of an unconfined sandy homogeneous aquifer, with a region of contamination near the capillary fiinge. This dimension was chosen to represent an existing laboratory model at Michigan State University. However, the numerical prototype can easily be modified to further this research. The contaminated region was modeled as a heterogeneous region in the aquifer due to the reduced relative permeability of the aqueous phase resulting from the trapped immobile immiscible phase. Values of the aqueous phase permeability were selected from the measured values in the ID column studies. Model simulation of a vertical cross section indicate that the reduced relative permeability in this region does not cause major by-passing. The optimum delivery and recovery of the surfactant was achieved when ‘maintaining local flow velocities near the range of ambient flow velocities prior to pumping. These low pumping rates maintained relatively horizontal flow paths in the aquifer. As a result, the 1-D model was used to evaluate the residence time to predict whether sufficient contact time was achieved. The ID and 2-D modeling indicate that surfactant can be delivered throughout the contaminated region and recovered from the aquifer using hydraulic controls which also promote sufficient contact time with the contaminated region. Through this research effort, an understanding of the interactive roles of rate- limited mass transfer in remediation, reduced relative permeability near the capillary fiinge, and the use of hydraulic controls near the capillary fiinge has been advanced. 152 Experimental methods and an implicit l-D numerical transport model were developed and used in conjunction with an existing 2-D code to evaluate the in-situ use of surfactant enhanced remediation of trapped residual NAPL near the capillary fiinge. This work is of interest to researchers in immiscible flow in porous media and in-situ aquifer remediation. 7.2. Summary of Costs This section is provided to give a general overview of the costs associated with the in-situ use of surfactant enhanced aquifer remediation. Roy F. Weston, Inc. (1988) outline additional design considerations, equipment requirements, treatment needs, disposal needs, monitoring requirements, pemiitting requirements, exposure pathways, environmental effectiveness and costs involved with in-situ leaching, which includes surfactant enhanced aquifer remediation, based on surveying past remediation. In the survey, the capital cost data is scarce, due to limited experience with these methods of remediation. As a result, the costs are limited to equipment needs which are summarized in Table 7 .1. The cost of surfactant (Witconol NP-150) is approximately $0.99 per pound. For a 5% solution of surfactant, the treatment costs are approximately $1 lO/m3. For the contaminated region evaluated (0.8 m x 0.3 m), one pore volume of treatment costs approximately $106 per unit width. 7 .3 Recommendations The following list overviews possible directions for future research based on the dissertation presented: . Investigate the lumped mass transfer coefficient for varying surfactant concentrations. . Investigate the use of SUTRA to predict the removal of an immobile phase while monitoring the concentration of the immobile phase. 153 . Develop or acquire a model that includes the transport of the miscible surfactant and the transport of an immiscible immobile phase in the surfactant enhanced aqueous phase. . Conduct a similar 2-D study for a less permeable soil to consider hydraulic controls in a region where slow velocities limit the optimum use of the surfactant to enhance the dissolution of trapped residual NAPL. . Extend the model aquifer region to include both a larger cross sectional area of the aquifer in addition to a larger contaminated region. . Investigate the effects of local heterogeneities caused by layers of clay and silt with respect to this study. . Conduct an experiment in the 2-D laboratory scale model to either qualitatively or quantitatively measure the size and shape of the discontinuous NAPL ganglia. In addition, measure the hydraulic conductivity in the 2-D setting. Current research is focused on predicting the mass transfer rate of NAPL into the aqueous phase based on measurable fluid or soil properties which may predict the changing size and shape of the residual NAPL blob. A study which evaluated the effect of surfactant concentration on the lumped mass transfer coefficient may contribute to the understanding of the dissolution process. SUTRA can include an immiscible contaminant, but does not track the changing volume of the immiscible phase in the output. In addition, it can not model both the transport of the surfactant enhanced - aqueous phase and the transport of the solubilized NAPL. A model may be available with these capabilities. The study should be expanded to investigate hydraulic controls in aquifers where the residence time is difficult to achieve. In a less permeable soil, the trapped residual NAPL may have a more pronounced effect on the flow within the aquifer, causing the surfactant enhanced aqueous phase within the contaminated region to solubilize dodecane at equilibrium solubility concentration during the initial migration of 154 the treatment into the region. Using the same aquifer material, a larger aquifer region should be studied based on similar reasoning. For the aquifer soil studied, the relative permeability of the soil is not reduced by the presence of trapped residual oil as significantly as localized clay and 'silt layers which should also be considered in a more realistic representation of in-situ environment. Past research in identifying ganglia size and shape has been in 1-D columns, where the column walls may limit the size of the ganglia, as suggested by the stable ganglia length calculations. The laboratory scale physical model could be used to measure ganglia in addition to measuring the hydraulic conductivity of the aquifer material and in the region of contamination. Item Description ‘ Approximate Cost“ Capital Costs Submersible pumps (wells) 50-2000 Centrifugal pump (chemical 8400-81000 feed) PVC pipe 0.15 m diameter $100-$600 Installation Costs PVC pipe $49.20-$65.60/m $65.6-$82/m Operation and Sampling and analytical costs 4 samples per year, 3 $49.2-865.6/m Maintenance monitoring wells Costs Table 7.1. Summary of costs in 1986 dollars involved with in-situ leaching (Roy F. Weston, Inc. 1988). ‘ Appendices Appendix A Analytical Solution to the 1-D Transport Equation (van Genuchten and Alves 1982) 6C 52C 6C R——=D — —— C+ a. 3x2 vé’x p y Initial and Boundary Conditions C(x,0)=C,- C 0 t t C(O,t)={ ° < < ° 0 (>10 6C ,1 =0 §_x(oo ) 1+[Q—Z)A(x,t)+[C-(x,—Z)Bt) 0to _# ll .11 where: Rx— vt 1 Rx+vt A(x, t): exp(- %t){l——etfn{2(0 INN-Sap )r2(DRt)i] B(x,=t) %exp[(u2v)x)] ]e Rx 2(DRm]+ +exp-;-[ [(u+v)x)]erf R2;3t,] i u: v[l+ 44120) v 155 Appendix B Implicit l-D Transport Code for Surfactant Enhanced Dissolution of an Irnmobile Residual NAPL PROGRAM MPLICIT tittttIfitttitittiiiiitfittt$ititi$#***********##*********************¥ LIZE'ITE R. CHEVALIER MICHIGAN STATE UNIVERSITY DEPARTMENT OF CIVIL AND ENVIRONMENTAL ENGINEERING 1994 l-D TRANSPORT CODE FOR SURFACT ANT ENHANCED DISSOLUTION OF A UNIFORM SATURATION OF TRAPPED RESIDUAL NAPL IN SATURATED SOIL *§§**§§**§§ tttittfitttttfi¥t#*##*##¢#***##tttttt**ttittt******###**tttittttttttttt *ttttttfittttttttttltttttttfi¢#***t***t*tttt00*#tttttttttttttttlttttfifit IMPLICIT CODE CENTERED DIFFERENCE FOR SPATIAL TERM FORWARD DIFFERENCE FOR TEMPORAL TERM TRIDIAGONAL MATRIX fifl'fittl'l‘l'l t*ttttttitttitt¥*tifittfitttt****#*#ttttittitttt¥t¥tt¥¢tttttttt*ttttfitt IMPLICIT DOUBLE PRECISION (A-H,O-Z) DIMENSION CANAL(5000),C(5000),E(5000),F(5000),G(5000) DIMENSION X(5000),R(5000) CHARACTERMO FILEl COMMON/CCN,RR,D,DX,RKL,CE,DT MARRAY=5000 fltitittttiltittttittttttttttttfitt##ttitttittitttfiltfiltltttfitttttttfitt t "' C-G-S UNITS ‘ . "' AREA = CROSS SECTIONAL AREA OF COLUMN * Q = FIJIJX 156 §§§§§§§§§Q§l>§ 157 = VELOCITY = POROSITY C(X) = CONCENTRATION OF NAPL IN AQUEOUS PHASE AT TIME T CA(X) = ANALYTICAL SOLN. OF NAPL CONC. IN AQUEOUS PHASE = MASS TRANSFER RATE COEFFICIENT CE = EQUILIBRIUM CONCENTRATION OF NAPL IN AQUEOUS PHASE GAMMA = DISPERSIVITY = DISPERSION = RETARDATION COUR = COURANT NUMBER DA = DAMKOHLER NUMBER RLENGTH = COLUMN LENGTH itit.t*ttttttitttttitttttfittttttttitittttt##tfit**¢*****¢*¥$¢t¥*¢¢tt it. it. PRINT *3 PROGRAM INITIATED' PRINT *: ENTER OUTPUT FILE NAME' READ(*,'(A40)°)FILE1 PRINT *,' ENTER (1) IF EVALUATING TOTAL POROSITY‘ ‘ PRINT *,' ENTER (2) IF EVALUATING EFFECTIVE POROSITY‘ READ(‘,*)LFLAG PRINT *3 ENTER ALPHA' READ(",")ALPHA PRINT *: ENTER COURANT NUMBER' READ(*,*) COUR PRINT #3 ENTER Dx (cm)' READ("',‘)DX PRINT ‘3 ENTER (1) IF DISPERSION INCLUDED IN NUMERICAL SOLN PRINT *,° ENTER (2) IF DISPERSION NOT INCLUDED READ(",") IFLAG PRINT I: ENTER DAMKOHLER NUMBER' READ(‘,*) DA PRINT t: ENTER LENGTH‘ READ(","‘) RLENGTH DATA (ml,g,cm) PRINT ‘,' ENTER ITIME' READ(*,"')ITIME I CO=0.0 AREA=23.24D0 DENSITYW=0.998D0 DENSITY O=0.75D0 RN=O.38DO RKL=0.387/60/60 CE=2000"0.7996 SRNI=0.18D0 RR=1 USER DEFINED DATA D=V‘0.136 IF(LFLAG.EQ.2)RN=RN‘(l-SRNI) V=RKL‘RLENGTH/DA Q=V*RN*AREA tit 10 23 158 QMIN=Q*6O DA=RKL*RLENGTH/V D=V‘O. 136 DT=COUR*DX/V NCELLS=RLENGTHIDX BETA=I-ALPHA SET INITIAL DISTRIBUTION DO 10 I=l,NCELLS C(I)=0.0DO IFCIFLAG.EQ.2)D=O Al=-2"‘ALPHA"'D*DT-V"ALPHA*DX*DT A2=2*DX’DX+4*ALPHA*D’DT+2“'ALPHA*RKL‘DX*DX*DT A3=2*ALPHA"D‘DT+V*ALPHA"DX‘DT Bl=2"RKL‘CE*DX*DX‘DT BZ=2‘BETA‘D‘DT+V*BETA*DX*DT B3=-2’RKL‘BETA*DX"DX*DT+2*DX‘DX-MBETA‘D‘DT B4=2*D‘BETA‘DT-V‘BETA‘DT‘DX D=V‘0. l 36 OPEN(5,FILE=FILE l) WRITE(5, 101) WRITE(5,102)DA,COUR WRITE(5, 104)V,RLENGTH WRITE(5,105)DX,DT WRITE(5, 106)NCELLS,QMIN WRITE(5, 103)ALPHA IF (IFLAG.EQ.2) WRITE(5,110) DO 20 J=l,ITIME DO 23 I=l,NCELLS CALL ASOLN(CA,I,I) CANAL(I)=CA IF(I.EQ.1) THEN F(I)=A2 G(I)=A3 R(I)=Bl+C(I)‘B3+C(I+l)"'B4-Al*CO GOTO 23 ENDIF IF(I.EQ.NCELLS)THEN E(I)=Al F(I)=A2+A3 R(I)=Bl+C(I-l)*BZ+C(I)*(B3+B4) GOTO 23 ENDIF E(I)=AI F(I)=A2 G(I)=A3 R(I)=Bl+C(I-l)"‘BZ+C(I)*B3+C(I+1)*B4 CONTINUE CALL TRI(E,F,G,X,R,NCELLS) 25 20 28 101 102 103 104 105 106 112 110 120 159 D0 25 I=l,NCELLS C(I)=X(D C(NCELLS+1)=C(NCELLS) CONTINUE TTIME=J*DT/60/60/24 WRITE(5,1 12)TI'IME DO 28 I=l,NCELLS XLOC=(DX*(I-l)+0.5*DX)/RLENGTH CA=CANAL(I)/CE CI=X(I)/CE ERROR=CANAL(I)-X(I) PER=ABS(ERROR/CANAL(I)* 100) NCOUNT=I+NCOUNT IF (NCELLSGT. 100) THEN IF(NCOUNT.EQ.10) THEN WRITE(5,120)XLOC,CA,CI,ERROR,PER NCOUNT=0 ENDIF ELSE WRITE(S, 120)XLOC,CA,C1,ERROR,PER ENDIF CONTINUE FORMATC COMPARING ANALYTICAL NUMERICAL SOLUTIONS',/, + ' IMPLICIT METHOD',/) FORMATc DA =',F6.3,' COUR =',F6.3) FORMATC ALPHA =',F6.3) FORMATc V(cm/sec) = ',F8.5,3X,' LENGTH (cm) = ',F8.1) FORMATC DELTA x (cm) = ', F8.3,3X,' DELTA T (sec) = ',F8.2) FORMATc NUMBER OF CELLS =’,I4,' Q (ml/min) = ',F8.3) FORMATC TOTAL TIME (days) ',F8.3//‘X/L CA C ERROR %°,/) FORMATc DISPERSION NOT IN NUMERICAL SOLN.') FORMAT(FS.3,2(1X,F5.3),1X,F8.3,1X,F10.3) PRINT *,' PROGRAM TERMINATED NORMALLY‘ 1000 END ttitttttitttfititttiittt*ttttittttfitt******¢***#***********t**#*#*¥* SUBROUTINE ASOLN(CA,I,J) IMPLICIT DOUBLE PRECISION (A-H,O-Z) COMMON/CC/V,RR,D,DX,RKL,CE,DT GAMMA=RKUCE TERM=GAMMA/RKL R=RR X=I*DX-0.5*DX T=J*DT CI=0.0D0 CO=0.0D0 DENOM=2*(D"'R*T)"*O.5 U=V‘(1+4*RKL*D/V“2)“O.5 160 AA4= l-ERF((R"X +V*T)/DENOM) IF(AA4.EQ.0)THEN A=DEXP(-RKL*T/R)*(1-0.5"'(l-ERF((R"‘X-V*T)/DENOM))) ELSE =DEXP(-RKL‘T/R)*(l-O.5*(l-ERF((R*X-V*T)/DENOM)) + -0.5*DEXP(V"‘X/D)"(l-ERF((R*X +V*”D/DENOM))) ENDIF BB4=l-ERF((R*X+U"‘T)/DENOM) IF(BB4.EQ.0)THEN B=0.5*DEXP((V-U)*X/2/D)*(I-ERF((R*x-U*T)/DENOM)) ELSE B=O.5‘DEXP((V-U)*X/2/D)*(l-ERF((R*X-U"T)/DENOM))+ + 0.5*DEXP((V+U)*X/2/D)*(l-ERF((R*X+U*T)/DENOM)) ENDIF CA=TERM+(CI-TERM)*A+(CO-TERM)*B RETURN END iitt***¥*¥#*tttiittfifitttt*********¥*¥****#it***##**************#**¥ DOUBLE PRECISION FUNCTION ERF(X) IMPLICIT DOUBLE PRECISION (A—H,O-Z) IF (X.EQ.0.0) THEN ERF=0.0 RETURN ENDIF IF (X.LT.0.0) THEN I=I x=-x ELSE I=0 ENDIF P=0.32759ll AI=0.254829592 A2=-0.284496736 A3=l.42141374l A4=-1.453152027 A5=1.061405429 T=l.O/(l.0+P"'X) ERF=1.o-(A1*T+A2*T**2+A3*T**3+A4*T**4+A5*T"5)* + DEXP(-X*X) IF(I.EQ.1) THEN ERF=-ERF =-x ENDIF RETURN END ##ttfittttififitt¥t#¢#¢¢*##**#*¥*tttt*#**#*************$¥¢**¥t*$$$*t*¥ tit 10 it? 20 ##t 30 161 SUBROUTINE TRI(E,F,G,X,R,N) IMPLICIT DOUBLE PRECISION (A-H,O-Z) DIMENSION E(5000),F(5000),G(5000),X(5000),R(5000) DECOMPOSITION DO 10 K=2,N B(KFE(K)/F(K-1) F(K)=F(K)-E(K)*G(K-1) CONTINUE FORWARD SUBSTITUTION DO 20 K=2,N R(K)=R(K)-E(K)*R(K-1) BACKWARD SUBSTITUTION X(N)=R(N)/F (N) DO 30 K=N-l,1,-l X(K)=(R(K)-G(K)*X(K+1))/F (K CONTINUE - RETURN END Appendix C Determination of Mass Transfer Coefficient-Output from SCIENTIST Sofiware The following tables were generated from the output of the software used to determine the lumped mass transfer coefficient, Scientist by MicroMath Scientific Sofiware (Salt Lake City, Utah). Table Cl.l. Output from Scientist Software used to determine mass transfer coefficient, k. = 0.387 hr'l. Goodness-of-fit statistics for data set Model A=A0(l-e'kt) Weighted Unweighted Sum of squared observations 11.258 11.258 Sum of square deviations 0.086 0.086 Standard deviation of data 0.064 0.064 R-sguared 0.992 0.992 Coefficient of determination 0.965 0.965 Confidence Intervals ’ Parameter name A0 Estimated value 0.7996 Standard Deviation 0.019 95% Range (Univar) 0.761 0.838 95% Range (S-plane) 0.751 0.848 Parameter Name K Estimated value 0.387 Standard Deviation 0.047 95% Range (Univar) 0.290 95% Range (S-plane) 0.264 162 163 Table Cl.l- continued. Variance-Covariance Matrix 0.084 -0.1 193 Correlation Matrix 1 .00 -0.565 Information from Residual Analysis: The following are normalized parameters with an expected value of 0.0 Values are in units of standard deviaton form the expected value. The serial correlation is 1.71 which indicates a systematic non-random trend in the residuals. Skewness is -1.58 indicating the likelihood of a few large negative residuals having an unduly large effect on the fit. Kurtosis is 0.06 which is probably not Significant. The weighting factor was 0.00 leading to a heteroscedacticity of -0.54 which suggests an optimal weight factor for this fit of ab0ut -O.54. 164 Table C1.2. Output from Scientist Software used to determine mass transfer coefficient, k. = 0.161 hr'l. Goodness-of-fit statistics for data set Model A=(1-e'kt) Weighted Unweighted Sum of squared observations 11.258 11.258 Sum of square deviations 0.307 0.307 Standard deviation of data 0.118 0.118 R-squared 0.972 0.972 Coefficient of determination 0.697 0.697 Correlation ~ 0.962 0.962 Confidence Intervals Parameter name K Estimated value 0.161 Standard Deviation 0.015 95% Range (Univar) 0.129 0.193 95% Range (S-plane) 0.129 0.193 Variance—Covariance Matrix: 0.017 Correlation Matrix: 1.00 Information fi'om Residual Analysis: The following are normalized parameters with an expected value of 0.0 Values are in units of standard deviaton form the expected value. The serial correlation is 3.33 which indicates a systematic non-random trend in the residuals. Skewness is -1.77 whichis probably not significant. Kurtosis is 0.08 which is probably not Significant. The weighting factor was 0.00 leading to a heteroscedacticity of -1.25 which suggests an optimal weight factor for this fit of about -1.25. Appendix D Summary of Input Data for SUTRA Model 165 3 we.» as. 225 B SEES 8 8 5mm .. .. 8% 85 E a 8323 5832 V22: _ _ 85:83; @0580 3:20 85 3o eou§8§32§ .5sz no 3 mam»? 888% 3885 .5 2: 8" :2 389223 B 88 E can: 5 2% 3 83> 96.5. ...... a... g 7 gm 200 ~+ amm— c o ugh 3385 o 3% 88am _+ Emm— _ _ >55 E225 o 2% 38a I 0.59 c _ 8.238 c 3839.5 1 e322 o c 893.88 3.. 89... Saw E .36.... 5252 82.2 c c 88.. 8:388 E .352 momz a c 3839. was 228 55 88.. B 5:32 . . :82 m e E3038 55 88.. E .352 momz o o .88 858% a? 88: B .352 252 a an 238a Reece. a? 88: B .8852 232 o c 5252 a :. 8N 8m 38%.» B .3552 5 an 88.. B exaaz EOE: 22> meeam .h—fio Egan .........,.._....,..w..u_a...»....H...,.....,..4.3m..m”..H.n.....n...._.,........«A»,an..h...n..,.u...a..uflmm..».fiwuw.flis.”...“.w.........“CHAIRMAN.,. : . . ...H.” ...... . .......... Ban—Em 3838:: w... . 22335 3582. SEE E 8...: 3.5 382 gm E 98 sea .8 3585 a xenon? AAQ might dos—5:8 - .80ng 10:08:: gm 5 com: San— AAD mama. 167 gigguvumaduofificuogagg a Sggggggo§> 9.. don—.mbmmD SE @023 dos—5:8 - macaw—25m flow—0:5: gm 5 com: San— ._ . a mama? Appendix E Materials and Suppliers Ottawa Sand Soiltest 86 Albrech Dr. PO. 8004 Lake Bluff, Illinois 50044-8004 Telephone: 1.800.323. 1242 Description: Ottawa density sand; p approximately 93 lb/ft3 (1.49 g/cm3) Dodecane Phillips 66 Company A Subsidary of Phillips Petroleum Box 968 Borger,Texas 79008-0968 Telephone: 806.274.5236 Description: Technical grade Witconol NP-l 50 WITCO 1 American Lane Greenwich, Connecticutt 06831 203.552.2000 Description: Product Code 087-5935 Oil Red 0 Biological Stain Aldrich Chemical Company PO. Box 355 Milwaukee, Msconsin 53201-9358 Telephone: 1.800.558.9160 Description: Stock # 19,819-6 168 List of References List of References Abdul, AS, Gibson, T.L., Ang, C.C., Smith, and J.C. Sobczynski. 1992. ”In-Situ Surfactant Washing of Polychlorinated Biphenyls and Oils from a Contaminated Site”, Ground Water, 30(2): 219-231. Abriola, L.M. 1989. "Modeling Multiphase Migration of Organic Chemicals in Groundwater Systems - A Review and Assessment”, Environmental Health Perspectives, 83:117-143. Amaefule, J .O. and LL. Handy. 1981. ”The Effect of Interfacial Tensions on Relative Oil-Water Permeabilities of Consolidated Porous Media", SPE/DOE 9783, presented at 1981 SPE/DOE Second Joint Symposium on Enhanced Oil Recovery, Tulsa, 0k, April 5-8. American Petroleum Institute. 1972. ”The Migration of Petroleum Products in Soil and Ground Water: Principles and Countermeasures", API Publication No. 4149. Anderson, R.L. 1987. Practical Statistics for Analytical Chemists, Van Nostrand Reinhold, pp.94-107. Anderson, MP. 1979. "Using Models to Simulate the Movement of Contaminants Through Groundwater Flow Systems", CRC Critical Reviews in Environmental Control, 9(2): 97-156. Anderson, MP. and W.W. Woessner. 1992. Applied Groundwater Modeling: Simulation of F low and Advective Transport, Academic Press. Ang, C.C. and AS. Abdul. 1991. "Aqueous Surfactant Washing of Residual Oil Contamination fi'om Sandy Soil”, Spring Gm, pp. 121-127. Battermann, G. 1986. "Decontamination of Polluted Aquifers by Biodegradation", Contaminated Soils, First International 7N0 Conference on Contaminated Soil, Edited by J. S. Assink and WJ. van den Brink, Martinus Nrjhofl‘ Publishers, Dordrecht, Netherlands. Bear, I. 1979. Hycb'aulics of Grounaivater, McGraw-Hill, New York, NY. 169 170 Bear, 1., Beijin, MS. and RR Ross. 1992. ”Fundamentals of Ground Water Modelling”, EPA/540/S-92/005. Berg, RR 1975. ”Capillary Pressures in Stratigraphic Traps”, AAPG Bull, 59(6):939- 956. Borden, RC. and C. Kao,. 1989. ”Water Flushing of Trapped Residual Hydrocarbon: Mathematical Model Development and Laboratory Validation“, Proceedings of the Conference on Petroleum Hydrocarbons and Organic Chemicals in Ground Water: Prevention, Detection and Restoration, NWWA, API, pp. 473-486. Chapra, SC and RP. Canale. 1988. Numerical Methods for Engineers, 2nd Edition, McGraw-Hill,. Chatzis, I., Morrow, NR, and HT. Lim. 1983. "Magnitude and Detailed Structure of Residual Oil Saturation”, SPEI, 23:311-326. Chatzis, I. and NR. Morrow. 1984. ”Correlation of Capillary Number Relationships for Sandstone”, SPEJ, 24(5):555-562. Chatzis, I, Kuntamukkula, MS, and NR Morrow. 1988. ”Effect of Capillary Number on the Microstructure or Residual Oil in Strongly Water-Wet Sandstones", SPE Reservoir Eng. , 3(3):902-912. Chatzis I. and PAL. Dullien. 1983. "Dynamic Immiscible Displacement Mechanisms in Pore Doublets: Theory Versus Experiment", J. Coll. Inter]? Sci, 91(1): 199-222. Clarke, AN, Mutch Jr., RD., Wilson, D.J., and KR Oma. 1992. ”Design and Implementation of Pilot Scale Surfactant Washing/Flushing Technologies Including Surfactant Reuse", Wat. Sci. Tech, 26(1-2):127-l35. Clarke, A.N., Plumb, P.D., Subramanyan, T.K., and D.J.\Vrlson. 1991. ”Soil Clean-Up by Surfactant Washing. 1. Laboratory Results and Mathematical Modeling”, Sep. Sci. Technol, 26(3): 301-343. Conrad, S.H., Wilson, J.L., Mason, WR. and WJ. Peplinski. 1992. ”Visualization of Residual Organic Liquid Trapped in Aquifers", Water Resour. Res, 28(1): 467-478. Conrad, SH, Hagan, ER, and J.L. Wilson. 1987. ”Why are Residual Saturations of Organic Liquids Different Above and Below the Water Table?”, Presented at NWWA/API Conference on Petroleum Hydrocarbons and Organic Chemicals in Ground Water - Prevention, Detection and Restoration. Corey, AT. 1984. Mechanics of Immiscible Fluids in Porous Media, Water Resources Publication. 171 Craig, F.F., Jr. 1971 The Reservoir Engineering Aspect of Waterflooding, Henry L. Hoherty Series: Monograph Volume 3, Society of Petroleum Engineers of American Institute of Mining, Metallurgical and Petroleum Engineers, N.Y. Edwards, DA. and RG. Luthy. 1990. "Nonionic Surfactant Solubilization of Polycych Aromatic Hydrocarbons in Aqueous and Soil/Water Systems”, Environmental Engineering, Proc. of the 1990 Specialty Conference, C.R. O'Melia, Ed., Arlington, Va. pp. 286-289. Ellis, W.D., Payne , JR, Tatum, AN., and F]. Firestone. 1984. "The Development of Chemical Countermeasures for Hazardous Waste Contaminated Soils", EPA/600/2-85/129. Ellis, W.D.,Payne, J.R., and GD. McNabb. 1985. ”Treatment of Contaminated Soils with Aqueous Surfactants”, EPA/600/2-85/129, NTIS PB 86-122 561/REB. Fischer, H.B., List, E.J., Koh, RC.Y., Imberger, J., and NH. Brooks. 1979. Mixing in Inland and Coastal Waters, Academic Press. Fountain, J.C. 1991. "Field Tests of Surfactant Flooding: Mobility Control of Nonaqueous-Phase Liquids”, Transport and Remediation of Subsurface Contaminants-Colloidal, Interfacial and Suflactant Phenomena, Edited by DA Sabatini and RC. Knox, pp. 182-191. Freeze, R. A. and IA. Cherry. 1979. Groundwater, Prentis Hall, Inc., Englewood Cliffs, NJ. Gilliland, HE. and FR. Conley. 1975. ”Surfactant Waterflooding", Proc. of the 9th World Petroleum Congress, Tokyo, Japan, May 11-16. Grubb, S. 1993. ”Analytical Model for Estimation of Steady-State Capture Zones of Pumping Wells in Confined and Unconfined Aquifers”, Ground Water, 31(1):27-32. Hall, CW. 1989. ”Practical Limits to Pump and Treat Technology for Aquifer Remediation”, Proceedings of Conference on Prevention and Treatment of Ground Water. Honarpour, M. Koederitz, L. and AH. Harvey. 1986. Relative Permeability of Petroleum Reservoirs, CRC Press. Hunt, JR, Sitar, N., and K.S.Udell. 1988. "Nonaqueous Phase Liquid Transport and Cleanup: 1. Analysis OfMechanisms”, Water Resour. Res, 24(8):]247-1258. Johnson, RE., and RH. Dettre. 1966. ”The Wettability of Low-Energy Liquid Surfaces", J. Coll. Interf Sci, 21, 610-622. 172 Keely, J .F. 1989. "Performance Evaluations of Pump and Treat Remediations", EPA/540/4-89/005. Klute, A. 1986. Methods of Soil Analysis, Part 1. Physical and Mineralogical Methods, American Society of Agronomy, Inc., Soil Science Society of American, Inc., Second Edition, Madison, WI. Knox, RC. and DA. Sabatini. 1991. "Transport and Remediation of Subsurface Contaminants”, Transport and Remediation of Subsurface Contaminants-Colloidal, Interfacial and Surfactant Phenomena, Edited by DA Sabatini and RC. Knox, pp. 1-1 1. _ Kueper, RH. and ED. Frind. 1988. "An Overview of Immiscible Fingering in Porous Media”, J. Contam. HydroL, 2: 95-110. Larson, RG., Davis, HT, and LE Scriven. 1981. ”Displacement of Residual Nonwetting Fluid fi'om Porous Media”, Chem. Eng. Sci, 36: 75-85. Levich, V.G. 1962. Physiochemical Hydrodynamics, Prentice Hall. Mace, RE. and J .L. Wilson. 1992. "Clay and Immiscible Organic Liquids: Greater Capillary Trapping of the Organic Phase”, Transport and Remediation of Subsurface Contaminants: Colloidal, Interfacial and Surfactant Phenomena, Edited by DA. Sabatini and RC. Knox, ACS Symposium Series No. 491:205-216. Mackay, D.M. and J .A Cherry. 1989. "Groundwater Contamination: Pump-and-treat Remediation”, Environ. Sci. T echnol. , 23 (6), 630-636. Mackay, D.M., Roberts, P.V., and J.A. Cherry. 1985. ”Transport of Organic Contaminants in Groundwater”, Environ Sci. Technol., 19(5):384-392. Melrose, J .C. and CF. Brandner. 1974. ”Role of Capillary Forces in Determining MicrOSCOpic Displacement Efficiency for Oil Recovery by Waterflooding", JCPT, 13(4): 54-61. Mercer, J .W. and RM. Cohen. 1990. "A Review of Immiscible Fluids in the Subsurface: Properties, Models, Characterization and Remediation”, J. Contain. Hydrol, 6: 107- 163. Miller, C.T., Poirier-McNeill, MM, and AS. Mayer. 1990. "Dissolution of Trapped Nonaqueous Phase Liquids: Mass Transfer Characteristics”, Water Resourc. Res., 26(1 1):2783-2796. Mohanty, K.K., Davis, HT, and LE. Scriven. 1981. ”Thin Films and Fluid Distribution in Porous Media”, Surface Phenomena in Enhanced Oil Recovery, Edited by DC. Shah, Plenum Press, pp. 595-609. 173 Morrow, NR and B. Songkran. 1981. "Effects of Trapping and Buoyancy Forces on Non-Wetting Phase Trapping in Porous Media”, Surface Phenomena in Enhanced Oil Recovery, Edited by DD. Shah, Plenum Press, pp. 387411. Morrow, NR, Chatzis, I., and H. Lim. 1985. "Relative Permeabilities at Reduced Residual Saturation”, JCPT, July-August, 24(4): 62-69. Morrow, NR, Chatzis, 1., and I]. Taber. 1988. ”Entrapment and Mobilization of Residual Oil in Bead Packs”, SPE Reservoir Eng, 3(3):927-912. Nash, J.H. and RP.Traver. 1984. ”Field Evaluation of In-Situ Washing of Contaminated Soils with Water/Surfactants", Proceedings of the Hazardous Material Spills Conference: Prevention, Behavior, Control and Cleanup of Spills and Waste Sites, April 9-12, Nashville, Tennessee. Nash, J.H. 1985. ”Field Studies of In-Situ Soil Washing”, Mason and Hanger - Silas Mason Company, EPA Contract No. 68-03-3203. Nash, J.H.. 1988. "Field Studies of In-Situ Soil Washing", EPA/600/SZ-87/110. Ng, K.M., Davis, HT and LE. Scriven. 1978. ”Visualization of Blob Mechanics in Flow Through Porous Media", Chemical Engr. Science, 33: 1009-1017. Palmer, CD. and W. Fish. 1992. ”Chemical Enhancements to Pump and Treat Remediation”, EPA/540/S-92/001. Parker, J .C. 1989. ”Multiphase Flow and Transport in Porous Meda", Reviews of Geophysics, 27(3):31 1-3 28. Pennell, K.D., Abriola, L.M., Dekker, T.J., and W.J. Weber. 1992. ”Surfactant Enhanced Solubilization of Entrapped Dodecane in Soil Columns”, American Chemical Society Division of Environmental Chemistry 203rd ACS National Meeting, San Francisco, 32(1):945-947. Pennell, K.D., Abriola, L.M., and W.J. Weber. 1993. ”Surfactant Enhanced Solubilization of Residual Dodecane in Soil Columns: 1. Experimental Investigation”, Environ. Sci. Technol., 27(12):2332-2339. Potter, MC. and DC. Wiggert. 1991. Mechanics of Fluids, Prentice Hall, Englewoord Clifl‘s, NJ. Powers, S.E., Abriola, L.M., and W.J. Weber. 1992. ”An Experimental Investigation of Nonaqueous Phase Liquid Dissolution in Saturated Subsurface Systems: Steady State Mass Transfer Rates”, Water Resourc. Res., 28(10): 2691-2705. Priddle, M.W., and K.T.B. MacQuarrie. 1994. "Dissolution of Creosote in Groundwater: An Experimental and Modeling Investigation”, J. Contam. Hydrol, 15:27-56. 174 Reichmuth, DR 1984. ”Subsurface Gasoline Migration Perpendicular to Ground Water Gradient - A Case Study”, Proceedings of the NWWA/API Conference on Petroleum Hycbocarbons and Organic Chemicals in Ground Water - Prevention, Detection and Restoration, Houston, Texas, pp. 43-52. Rosen, MJ. 1989. Surfactants and Interfacial Phenomenon, 2nd Ed, John Wiley and Sons. Roy F. Weston Inc. 1988. Remedial Technologies for Leaking Underground Storage Tanks, Lewis Publishers, pp. 55-63. Sale, T.C., Piontek, KR, and M.Pitts. 1989. ”Chemically Enhanced In Situ Soil Washing”, Proceedings of the Petroleum Hydrocarbons and Organic Chemicals in Groundwater:Prevention, Detection and Restoration, pp. 487-503. Schlitt, W.J., and DA Shock. 1979. ”In Situ Uranium Mining and Groundwater Restoration”, Proc. of the New Orleans Symposium, Solution Mining Committee, Society of Mining Engineers of American Institute of Mining, Metallurgical and Petroleum Engineers. Schmelling, S.G. 1992. "An Overview of Aquifer Remediation: NAPLS, Pump and Treat and Bioremediation", Subsurface Contamination by Immiscible Fluids, K.U. Weyer, Ed, AA Balkema/Rotterdam/Brookfield, pp. 39-45. Schwille, F. 1988. Dense Chlorinate Solvents in Porous and Fractured Media: Model Experiments, Translated from German by J.F . Pankow, Lewis Publishers, Chealsea, Michigan. Sherwood, T.K., Pigford, R.L., and CR Wilke. 1975. Mass Transfer, McGraw-Hill. Soeryantono, H., Wallace, RB., and TC. Voice. 1994. ”Acceptability of Pressure Equilibrium Method”, Draft, Michigan State University, Department of Civil and Environmental Engineering. Souza, WR 1987. Documentation of a Graphical Display Program for the Saturated- Unsaturated Transport (SUTRA) F inite-Element Simulation Model, U.S.G. S. Water-Resources Investigations Report 87-4245. van der Heijde, P.K.M., El-Kadi, AL, and SA Williams. 1988. ”Groundwater Modeling: An Overview and Status Report", EPA/600/2-89/028. van Genuchten, MT. 1980. ”A Closed Form Equation for Predicting the Hydraulic Conductivity of Unsaturated Soils”, Soil Sci. Soc. Am. J., 44:892-898. van Genuchten, MT. and W.J. Alves. 1982. Analytical Solutions of the One- Dimensional Convective-Dispersion Solute T ransprot Equation, U.S.G.S. Technical Bulletin No. 1661, 149 p. 175 Verschueren, K. 1983. Handbook of Environmental Data on Organic Chemicals, 2nd Ed, Van Nostrand Reinhold, pp. 595-596. Voss, CL 1984. A F mite-Element Simulation Model for Saturate- Unsaturated F luid- Density-Dependent Groundwater Flow with Energy Transport or Chemically- Reactive Single-Species Solute Transport, USGS Water-Resources Investigation Report 84-43 69. Wang, HF. and MP. Anderson. 1982. Introduction to Groundwater Modeling: Finite Drflerence and Finite Element Methods, W.H. Freeman. Wardlaw, NC. 1982. "The Effect of Geometry, Wettability, Viscosity, and Interfacial Tension on Trapping in Single Pore-Throat Pairs”, J. Can. Petrol. Tech, 21(3):21- 27. Weber, W.J.,Jr., McGinley, PM, and L.M. Katz. 1991. ”Sorption Phenomena in Subsurface Systems: Concepts, Models and Effects of Contaminant Fate and Transport", Water Res., 25(5):499-428. Wheatcraft, SW. and F. Winterberg. 1985. "Steady State Flow Passing Through a Cylinder of Permeability Different From the Surrounding Medium", Water Resourc. Res., 21(12):]923-1929. Wilson, J .L. and SH. Conrad. 1984. ”Is The Physical Displacement of Residual Hydrocarbons a Realistic Possibility in Aquifer Restoration”, Proceedings of Conference on Petroleum Hydrocarbons and Organic Chemicals in Ground Water, NWWA, Houston, Tex., , Nov. 1984, pp. 274-298. “Wilson, J.L., Conrad, S.H., Hason, WR, Peplinski, W., and E. Hagen,. 1990. ”Laboratory Investigation of Residual Liquid Organics fi'om Spills, Leaks, and the Disposal of Hazardous Wastes in Groundwater”, EPA/600/6-90/004. Mlson, DJ. 1989. "Soil Clean Up by In-Situ Surfactant Flushing. 1. Mathematical Modeling”, Sep. Sci. T echnol., 24(11): 863-892. Wilson, J.L. 1994. "Visualization of Flow and Transport at the Pore Level”, Transport and Reactive Processes in Aquifers, Th. Dracos and F. Staufl‘er, Eds, Rotterdam; Balkema. “Witco. 1991. Facsimile received from WITCO MPO ORG SLS, Nov. 26, 1991. Zalidis, G.C., Annable, M.D., Wallace, RB., Hayden, N.J., and TC. Voice. 1991. "A Laboratory Method for Studying the Aqueous Phase Transport of Dissolved Constituents from Residually Held NAPL in Unsaturated Soil Columns”, J. Contam. Hydrol, 8:143-156. ”’IlllilllIIIIIII‘“