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It 1 u t L £3 £1- i . l...i?2!3x.)lr 1.13 ‘I5\..i.. 3.1.57...‘ 99.3.5. .uuFEh-d ._{ EL... .. . . .32. : mists .q/(yo’v This is to certify that the thesis entitled Estimating Natural Attenuation Rates for a Chlorinated Hydrocarbon Plume in a Glacio-fluviai Aquifer, Schoolcraft, Michigan presented by Brian Andrew Lipinski has been accepted towards fulfillment of the requirements for MaSter'S degree in GCO'OQY Major professor Date January 21, 2002 0-7639 MS U is an Affirmative Action/Equal Opportunity Institution LIBRARY Michigan State University PLACE IN RETURN Box to remove this checkout from your record. TO AVOID FINES return on or before date due. MAY BE RECALLED with earlier due date if requested. DATE DUE DATE DUE ' DATE DUE 6/01 cJCIRC/DateDuepas-sz ESTIMATING NATURAL ATTENUATION RATES FOR A CHLORINATED HYDROCARBON PLUME IN A GLACIO-FLUVIAL AQUIFER, SCHOOLCRAFT, MICHIGAN By Brian Andrew Lipinski A THESIS Submitted to Michigan State University in partial fulfillment of the requirements for the degree of MASTER OF SCIENCE Department of Geological Sciences 2002 ABSTRACT ESTIMATING NATURAL ATTENUATION RATES FOR A CHLORINATED HYDROCARBON PLUME IN A GLACIO-FLUVIAL AQUIFER, SCHOOLCRAFT, MICHIGAN By Brian Andrew Lipinski A plume of chlorinated hydrocarbons in Schoolcrafi, Michigan, that has undergone abiotic and biotic degradation processes, was examined using numerical modeling techniques. The flow field was simulated with a three-dimensional steady state heterogeneous plume scale model that incorporated natural hydrologic boundaries through a Telescopic Grid Refinement of a three-dimensional steady state regional scale model that was extended to natural hydrologic boundaries. Contaminant plume evolution was examined using an RT3D model that includes. aerobic and anaerobic biodegradation of the source compounds PCE, TCE, TCA, and their daughter byproducts, as well as the simultaneous abiotic degradation of TCA. The model was used to estimate the degradation rates of the plume species by comparing the calculated ratio of a species to its daughter byproduct for observed data and simulated results in a well transect downgradient of the source. The ratio approach should be applicable to any field site in which contaminants degrade to form a byproduct, thus circumventing the source term problem. The plume compounds degraded at a rate between 10'2 day’1 and 10'5 day", which is similar to natural attenuation rates at the RTDF Dover Site. The rates are too slow to allow natural attenuation process alone to remediate the plume in a reasonable time frame. ACKNOWLEDGEMENTS Many people have contributed to the completion this thesis, and their help was greatly appreciated. First, I would like to thank the members of my committee. My advisor, Dave Hyndman, has provided much support and many insightfiil comments that led to the completion of the thesis. Committee members Gary Wiessmann and Dave Wiggert made significant contributions to the manuscript, which made the text flow much better, while also pointing out fundamental problem areas of the work. Jaime Graulau-Santiago helped with the assimilation of the plume data; his help was irreplaceable. The research was funded by the Michigan Department of Environmental Quality (contract #Y43086). There were also many people that made my stay here enjoyable and/or were very helpful. A short list includes Joel, Nick, Linker, Moss, and Chris. Maybe we will actually catch some steelhead on the Manistee River someday instead of just catching a cold. Also, we need to practice blackjack before we head back to Reno (note to self, always double down when you are dealt two aces). I would also like to thank Jackie, Cathy, and Loretta. Without their guidance, I would still have years left to finish my degree. Lastly, a good fi'iend once told me that I was not allowed back in Pennsylvania until I had completed my thesis. Well, it’s done, so I guess I can get back into the Keystone state. iii TABLE OF CONTENTS LIST OF TABLES ................................................................................ vii LIST OF FIGURES .............................................................................. viii I. INTRODUCTION AND SCOPE OF WORK .............................................. 1 OVERVIEW ...................................................................................... 1 SCOPE OF WORK ............................................................................... 8 II. THREE-DIMENSIONAL REGIONAL STEADY STATE GROUNDWATER FLOW MODEL OF SCHOOLCRAFI‘, MICHIGAN ........... 10 INTRODUCTION .............................................................................. 1 O PREVIOUS WORK ............................................................................ 11 Regional Geology ........................................................................... 12 Regional H ydrogeology ................................................................... 1 9 Regional Hydrology ........................................................................ 21 CONCEPTUAL MODEL ..................................................................... 22 Conceptual Boundaries ................................................................... 22 Conceptual Layers ......................................................................... 24 ARCVIEW ANALYSIS ....................................................................... 28 Boundary Digitization in Arc View ....................................................... 28 Stratigraphic Unit Development ......................................................... 29 IMPLEMENTATION OF THE CONCEPTUAL MODEL .............................. 33 Development of a 3-D Finite Difference Grid .......................................... 33 Layer Elevation Interpolation ............................................................ 34 Model Boundary Assignment ............................................................. 35 Hydraulic Conductivity Assignment ..................................................... 35 MODEL CALIBRATION ..................................................................... 38 Observed Head Data Set .................................................................. 38 Results ....................................................................................... 39 Discussion ................................................................................... 39 III. THREE-DIMENSIONAL PLUME SCALE STEADY STATE GROUNDWATER FLOW MODEL OF SCHOOLCRAFI‘, MICHIGAN ............45 iv INTRODUCTION .............................................................................. 45 CONCEPTUAL MODEL ..................................................................... 45 Conceptual Boundaries .................................................................... 45 Conceptual Aquifer Material Types ...................................................... 46 IMPLEMENTATION OF THE CONCEPTUAL MODEL .............................. 50 Development of a 3-D Finite Difference Grid .......................................... 51 Creation of Aquifer Solid Materials in GMS ........................................... 51 Interpolation of the Aquifer Solids to the MODFLOW Grid ......................... 51 Boundary Assignment ..................................................................... 55 MODEL CALIBRATION ..................................................................... 55 Results ....................................................................................... 55 Discussion ................................................................................... 56 IV. THREE DIMENSIONAL REACTIVE TRANSPORT MODEL OF PLUME G, SCHOOLCRAFT, MICHIGAN ................................................ 60 INTRODUCTION .............................................................................. 6O ARCO SITE BACKGROUND ............................................................... 60 Source Areas ................................................................................ 61 Previous Remediation Systems ............................................................ 63 DEGRADATION PROCESSES ............................................................. 66 Abiotic Degradation Processes .......................................................... 68 Biotic Degradation Processes ............................................................ 68 Biotic Degradation Process: Occurrence Under Aerobic Conditions .......... 69 Biotic Degradation Processes: Occurrence Under Anaerobic Conditions .............................................................................. 7O Biotic Degradation Processes: Rate Sensitivity to Redox Conditions ......... 71 CURRENT METHODS TO ESTIMATE FIELD SCALE DEGRADATION RATES ..................................................................... 71 Tracer normalization ...................................................................... 71 Semi-Graphical Method of Buscheck and Alcantar (1995) ........................... 73 Numerical Modeling ...................................................................... 74 Method to Estimate Rates at Plume G ................................................... 75 CONCEPTUAL MODEL ..................................................................... 75 Model Stress Periods ...................................................................... 75 Conceptual Reactions of Interest ......................................................... 79 Conceptual Method of “Calibration ” ................................................... 82 IMPLEMENTATION OF THE CONCEPTUAL MODEL .............................. 88 Creation of an RT 3D Reactions Package ............................................... 88 Assignment of Model Parameters ........................................................ 91 MODEL CALIBRATION ..................................................................... 94 Results .................................................................................... 95 Model Sensitivity to Degradation Rates ................................................ 98 Discussion ................................................................................. 1 08 SIGNIFICANCE AND APPLICATIONS ................................................. 109 Novel Aspects of the Model .............................................................. 109 Applications of the Research at the Site ............................................... 110 RECOMMENDATIONS FOR FUTURE WORK ....................................... 110 APPENDIX A. WELL LOG DESCRIPTIONS FOR MSU WELLS 1-9 ............. 114 APPENDIX B. 3-D SOLID STRATIGRAPHY MODELING IN GMS ............... 117 INTRODUCTION ............................................................................ l 17 GMS BOREHOLE DATA ANALYSIS ................................................... 117 TRIANGULAR INTERPOLATED NETWORKS ...................................... 118 CREATION OF 3-D SOLID OBJECTS ................................................... 118 REFERENCES .................................................................................... 124 vi TABLE 1 TABLE 2 TABLE 3 TABLE 4 TABLE 5 TABLE 6 TABLE 7 TABLE 8 TABLE 9 TABLE 10 TABLE 11 TABLE 12 TABLE 13 LIST OF TABLES Chemicals comprising each of the seven currently identified plumes in the Village of Schoolcrafl, Michigan (modified from Mayotte, 1991) ............................................. Hydraulic conductivities of the various materials in the regional model ........................................................................... Qualitative description of the materials comprising the aquifer in the plume scale model domain ............................................. Physical characteristics of the plume scale groundwater flow model (all cells were active) .................................................. Hydraulic conductivity data (K) for the different aquifer materials described in Table 3 (observed data from Mayotte, 1991 ) .................................................................. Summary of conceptual stress periods for plume G transport models ........................................................................... Estimated total aqueous mass of observed compounds at well transect in shallow (0-13 mbgs, 1.44x105 L), middle (13-19 mbgs, 1.36x105 L), and deep (19-27 mbgs, 1.07x105 L) zones for June of 1988 ................................................................. Summary of transport model parameters which remained constant throughout model calibration ....................................... Estimated source concentrations for the model source areas based on site investigation results assimilated in Everett (1990) ........ Summary of first order decay rates for chlorinated compounds as compiled by Suarez and Rifai (1999) .................................... Observed and simulated masses for the three conceptual contamination zones outlined in the Conceptual Calibration section . . Observed and simulated contaminant mother/daugher ratios for the three conceptual contamination zones outlined in the Conceptual Calibration section ............................................. Summary of calibrated parameters used in the RT3D model vii ..... 4 ...42 ...47 ...50 ...56 ...79 ...85 ...92 ...93 ....94 96 ...97 .97 LIST OF FIGURES FIGURE 1 Location of the Village of Schoolcraft, Kalamazoo County, Michigan ............................................................................. 2 FIGURE 2 Location and extent of MDNR plumes A-G in the Village of Schoolcraft (modified from Mayotte, 1991). Note the location of the John A. Biewer wood treatment facility and ARCO Industries Co., which are the source areas for plumes F and G respectively ....................................................................... 3 FIGURE 3 Bedrock map of the Lower Peninsula of Michigan with Kalamazoo County enlarged (modified Milstein, 1987). Note that the Coldwater Shale is Chartreuse, while the Marshall Formation is gray. Image is presented in color ..................... 13 FIGURE 4 Map of moraines in southwest Michigan and the study area of Monaghan et. a1. (1986). Note the location of the interlobate boundary that separates deposits of the Michigan Lobe from deposits of the Saginaw Lobe (modified from Monaghan et. al., 1986) ........................................................................ 14 FIGURE 5 Surficial map of Kalamazoo County (modified from Monaghan and Larson (1982) in Rheaume (1990)). Image is presented in color ............................................................... 16 FIGURE 6 Michigan Lobe tills correlated to respective moraine(s) in southwest Michigan (modified from Monaghan et. al., 1986). Schoolcraft lies between the Outer Kalamazoo Moraine and the Tekonsha Moraine of the Michigan Lobe ................................. 17 FIGURE 7 Map showing the approximate boundary of the F inkbeiner (1994) study area (modified from F inkbeiner, 1994). Note the trace of the Tekonsha Moraine, which is discussed in the text .............. 18 FIGURE 8 Location of the Prairie Ronde Fan presented by Steinmann (1994) (modified from Kehew et. al., 1996) ................................... 20 FIGURE 9 Location of the significant surface water bodies in the vicinity of Schoolcraft, Michigan that served as boundaries in the regional model. The perimeter boundaries that are not hydrologic boundaries are no flow boundaries interpreted as topographic divides from the DEM ............................................. 23 viii FIGURE 10 FIGURE 11 FIGURE 12 FIGURE 13 FIGURE 14 FIGURE 15 FIGURE 16 FIGURE 17 FIGURE 18 FIGURE 19 FIGURE 20 FIGURE 21 Simplified cross-section of the regional geology surrounding Schoolcrafi used to conceptualize the regional model. Figure layer thicknesses do not represent actual layer thicknesses. Image is presented in color ....................................................... 26 Flow chart outlining the steps taken to develop the regional model in the conceptual model process and summary of the results ............................................................................... 27 A) Location of the water wells near the regional model. B) Wells remaining after quality checks were performed, which are also sorted according to whether the layer 2 till was identified at the location .................................................... 31 Areal extent of the various conductivity zones used in the regional groundwater flow model (layer 1 is the top, layer 3 is the bottom) ...................................................................... 32 Variogram for interpolation of layer 1 bottom elevations ................... 36 Variogram for interpolation of layer 2 bottom elevations ................... 36 Interpolated model layer bottom elevations. The location of the data points from which elevations were interpolated are shown as triangles ................................................................. 37 Simulated vs. observed heads for the observation wells in the vicinity of Schoolcraft ........................................................ 40 Head distribution of the calibrated regional model (view is of the top layer) .................................................................... 41 Head distribution of the calibrated regional model with flow vectors to show direction of groundwater movement predicted by the model (view is of the top layer) ............................. 43 Location and orientation of the plume scale model in reference to the regional model (cells are not shown as they are too small to be seen at the current scale). Well locations are given for NUS and MSU wells where lithologic data were available for aquifer characterization ....................................................... 48 A) Contour map of the bottom of the plume scale flow model, which is also the bottom of layer 1 in the regional model. B) Contour map of the ground elevations in the plume scale flow model. The contour interval is 0.5 m ..................................... 49 ix FIGURE 22 Selected cross-sections through the 3-D GMS solids that represent the aquifer materials in the plume scale model. The locations of the wells used to create the solids are given on the inset. Image is presented in color (VE = 20X) ........................ 53 FIGURE 23 Graphical depiction of the results of the three GMS algorithms to map solid material properties to a hypothetical MODFLOW model. A) An arbitrary set of solids. B) Cross- section through A) using Boundary Overlay. C) Cross- section through A) using grid Overlay. D) Plan view of layer in A) showing the smoothing effects of Grid Overlay with Keq (modified from BYU, 2000). Image is presented in color ................... 54 FIGURE 24 Head distribution of the top layer of the calibrated plume scale model, which shows flow is in a southeasterly direction. The local heads are shown in grayscale, while the regional heads are superimposed in black. Inspection between the two distributions reveals a reasonable match ....................................................... 57 FIGURE 25 Plot of simulated vs. observed heads for the plume scale and regional scale model ............................................................... 58 FIGURE 26 Location of the five suspected source areas on the ARCO property (modified from Everett, 1990) ........................................ 62 FIGURE 27 Location of the three purge wells that were part of the initial pump and treat system to remediate plumes F and G (modified from Mayotte, 1991) ................................................. 65 FIGURE 28 Biotic and abiotic transformations of PCB, TCE, and TCA under aerobic and anaerobic conditions (modified from McCarty, 1997; and Bedient et. al., 1999). All transformations are biotic unless indicated with a dotted arrow, which is the abiotic pathway. Heavy arrow indicates preferential reaction .............. 67 FIGURE 29 Nitrate concentrations at monitoring well MSU-5 from February, 2001. Note that nitrate starts to decrease at about 13 mbgs until about 19 mbgs, where it remains constant. Results suggest that the aquifer is aerobic from the water table to 13 mbgs, anaerobic denitrifying from 13 mbgs to 19 mbgs, and somewhat more anaerobic from 19 mbgs to the clay at 26-27 mbgs ......................................................................... 81 FIGURE 30 Location of downgradient monitoring well transect used to identify vertical zones of contamination. The numbers correlate to the NUS number assigned to the wells during the remedial FIGURE 31 FIGURE 32 FIGURE 33 FIGURE 34 FIGURE 35 FIGURE 36 investigation studies in the late 1980’s (Mayotte, 1991) ..................... 86 Plot of TCE concentrations at a well transect perpendicular to groundwater flow approximately 650 meters downgradient of the ARCO facility. The shaded regions are the shallow, middle, and deep generalized zones of contamination. The view is looking upgradient towards ARCO. Image is presented in color .............................................................................. 87 Sensitivity plots of model error (RMSE) of the mother/daughter ratios (PCB/TCE path) in response to varying degradation rates (model rate is circled). A) The anaerobic PCE rate in the middle zone. B) The anaerobic PCE rate in the deep zone (note, PCE is not currently known to degrade under aerobic conditions, therefore there is no aerobic PCE rate in the shallow zone) ........................................ 100 Sensitivity plots of model error (RMSE) of the mother/daughter ratios (PCB/TCE path) in response to varying degradation rates (model rate is circled). A) The aerobic TCE rate in the shallow zone. B) The anaerobic TCE rate in the middle zone. C) The anaerobic TCE rate in the deep zone .......................................................................... 101 Sensitivity plots of model error (RMSE) of the mother/daughter ratios (PCB/TCE path) in response to varying degradation rates (model rate is circled). A) The aerobic 1,2-DCE rate in the shallow zone. B) The anaerobic 1,2-DCE rate in the middle zone (dashed line is where 1,2-DCE rate cannot be less than the VC rate in this zone). C) The anaerobic 1,2-DCE rate in the deep zone ..................................... 102 Sensitivity plots of model error (RMSE) of the mother/daughter ratios (PCB/TCE path) in response to varying degradation rates (model rate is circled). A) The aerobic VC rate in the shallow zone (dashed line is literature value boundary). B) The anaerobic VC rate in the middle zone (dashed line indicates VC cannot be higher than deep zone. C) The anaerobic VC rate in the deep zone (dashed line represents boundary where the VC rate in the deep zone cannot be lower than the middle zone ......................................... 103 Sensitivity plots of model error (RMSE) of the mother/daughter ratios (TCA path) in response to varying degradation rates (model rate is circled). A) The aerobic TCA rate in the Shallow zone. B) The anaerobic TCA rate in the xi FIGURE 37 FIGURE 38 FIGURE 39 middle zone. C) The anaerobic TCA rate in the deep zone ............ Sensitivity plots of model error (RMSE) of the mother/daughter ratios (TCA path) in response to varying degradation rates (modeled rate is circled). A) The aerobic DCA rate in the shallow zone. B) The anaerobic DCA rate in the middle zone (dashed line indicates the rate in the middle zone cannot be higher than in the deep zone). C) The anaerobic DCA rate in the deep zone .................................................. Sensitivity plots of model error (RMSE) of the mother/daughter ratios (TCA path) in response to varying degradation rates (modeled rate is circled). A) The aerobic 1,1-DCE rate in the Shallow zone. B) The anaerobic 1,1—DCE rate in the middle zone (dashed line indicates the 1,1-DCE rate cannot be lower than the VC rate in this zone). C) The anaerobic 1,1-DCE rate in the deep zone ................................. Sensitivity plots of model error (RMSE) of the mother/daughter ratios (TCA path) in response to varying degradation rates (model rate is circled). A) The aerobic VC rate in the shallow zone (dashed line is literature value boundary). B) The anaerobic VC rate in the middle zone (dashed line indicates VC cannot be higher than deep zone. C) The anaerobic VC rate in the deep zone (dashed line represents boundary where the VC rate in the deep zone cannot be lower than the middle zone ..................................... FIGURE B-l Location of the solid for which an explanation of 3-D solid FIGURE B-2 Location of the wells used to create the TINS and solids in GMS . . . . . construction in GMS is presented in Appendix B. The inset shows the areal extent of the solid with respect to the local model grid and in reference to the cross-sections. Image is presented in color (VE = 20X) ............................................. FIGURE B-3 Generalized steps of solid construction from a set of borehole objects in GMS. A) Creation of a TIN representing the top of a solid. B) Creation of a TIN representing the bottom of a solid. C) Top TIN with the interior nodes snapped to the bottom TIN. D) Resulting solid created by filling between C) and B). Image is presented in color ......................... xii ....104 ....105 ....106 ....107 ....120 121 ....122 CHAPTER I INTRODUCTION AND SCOPE OF WORK OVERVIEW The village of Schoolcraft is located in Kalamazoo County Michigan (Figure l). The town is a rural community with several small industrial sites. The activities at these sites are the focus of research currently being conducted at Michigan State University. Groundwater from the glacio-fluvial aquifer in the region is the primary source of drinking and irrigation water for the farmers (Mayotte, 1991); therefore, contamination of the aquifer is a severe threat to the livelihood of the community. Several contaminant plumes were identified in the aquifer beneath Schoolcraft in the 1970’s and 1980’s. A plume of hexavalent chromium and arsenic was discovered in the mid 1970’s and the Michigan Department of Natural Resources (MDNR) identified the source to be the John A. Biewer Company wood treatment facility. In 1985, the MDNR determined that the aquifer was contaminated with several chlorinated aliphatic hydrocarbons and ARCO Industries was identified as one of the sources. Subsequently, Halliburton NUS Environmental Corporation was hired in December of 1986 by the MDNR to identify and define all sources/plumes of contamination in the aquifer in and around the village. NUS determined that there were seven plumes in the aquifer beneath Schoolcraft. The plumes were named A-G (Figure 2) and a brief list of the chemicals contained within each one is given in Table 1 (Mayotte, 1991). The groundwater contamination at Schoolcrafi is part of an international problem. Chlorinated organic compounds, such as tetrachloroethene (PCE), trichloroethene (TCE), 42° 25' 040 I——l km I Kalamazoo Figure 1. Location of the the Village of Schoolcrafi, Kalamazoo County, Michigan. ELIZA ST WEST AVE ARCO l4"I STREET BIEWER Figure 2. Location and extent of MDNR plumes A-G in the Village of Schoolcraft (modified from Mayotte, 1991). Note the location of the John A. Biewer wood treatment facility and ARCO Industries Co., which are the source areas for plumes F and G respectively. and trichloroethane (TCA), gained widespread use in industry throughout the 20th century mainly in the form of solvents to degrease metals and machinery and in the dry cleaning industry. These chlorinated organic solvents have become ubiquitous groundwater contaminants throughout the United States and other countries through their subsequent misuse and mishandling (Jackson and Dwarakanath, 1999). PCE, TCE, and TCA are currently regulated by the Clean Water Act with Maximum Contaminant Levels (MCL’S) of 5 ppb, 5 ppb, and 200 ppb respectively because they are suspected human carcinogens. Another problem is that these compounds undergo a series of dechlorination reactions to form compounds such as dichloroethene (DCE), dichloroethane (DCA), and vinyl chloride (VC). All of these compounds are suspected carcinogens and have MCL’s as follows: 1,1-DCE (7 ppb), cis-1,2-DCE (70 ppb), trans-1,2-DCE (100 ppb), 1,1-DCA (70 ppb), and VC (2 ppb). The transformation of PCB, TCE, and TCA to their daughter by- products is a topic that has been heavily researched in the literature, a review of which is given by Vogel (1987) and further by Semprini et. a1. (1995). Table 1. Chemicals comprising each of the seven currently identified plumes in the Village of Schoolcraft, Michigan (modified from Mayotte, 1991). Plume Contaminants Present carbon tetrachloride, chloroform, trichloroethane, and trichloroethene benzene and 1,2-dichloroethene trichloroethane, trichloroethene, and methylene chloride tetrachlorethene, trichloroethene, and trichloroethane tetrachloroethene, trichloroethene, and trans-1,2-dichloroethene arsenic and hexavalent chromium tetrachlorethene, trichloroethene, and trichloroethane Gremcnw> Significant attention in government, academia, and private consulting has focused on developing successful remediation strategies due to widespread contamination of groundwater with PCE, TCE, and TCA. One of the most common remediation methods is with “pump and treat”. In a pump and treat system, several wells are typically installed downgradient of the source area and pumped in a manner as to “capture” the contaminated groundwater. The captured water is pumped to the surface and directed to some type of wastewater treatment facility (Fetter, 1993). The treatment facility consists of either an air stripping tower, a reaction vessel, or a combination of both. The air stripping tower contains a packing material onto which contaminated water is sprayed as air is forced through the tower. The organic compounds volatilize as air passes over the packing material and the vapors are carried out the top of the tower to the atmosphere. If the contaminant is not very volatile, the captured water is treated with a reaction vessel. The reaction vessel contains granular activated carbon (GAC) onto which the contaminants will sorb (Driscoll, 1986). The treated wastewater must then be disposed. Several drawbacks exist to the pump and treat approach. First, the systems are typically in operation for a significant time-period and they pump excessive volumes of water, both of which are very costly endeavors. Second, contaminants that have diffused into the low conductivity zones are difficult to remove because pumping preferentially draws water from the high conductivity zones. In addition, the sorbed phase of the contaminant may not be removed from the aquifer matrix (Fetter, 1993). Also, air shipping only acts to transfer the contaminant to the atmosphere which potentially creates an air pollution problem. Lastly, the extracted water must be disposed, which may require federal and state permits (Fetter, 1993). For these reasons, alternative methods of aquifer treatment have been sought. In-situ bioremediation is a method of contaminant remediation that has recently gained popularity. The general principle is that microbes will directly or indirectly break down the undesired chemical to harmless by-products, which is a much more desirable result than the end product of pump and treat systems. There are currently three general sub-categories of bioremediation: monitored natural attenuation (MNA), biostimulation, and bioaugrnentation. MNA is referred to by many other names, such as intrinsic bioremediation, passive remediation, or natural recovery (Azadpour-Keeley et. al., 2001). Natural attenuation processes include degradation, dispersion, and sorption. The United States Environmental Protection Agency (USEPA, 1997) defines MNA as ...the reliance on natural attenuation processes to achieve site- specific remedial objectives within a time frame that is reasonable compared to other methods. The “natural attenuation processes ” that are at work in such a remediation approach include a variety of physical, chemical, or biological processes that under favorable conditions, act without human intervention to reduce mass, toxicity, mobility, volume, or concentration of contaminants in soil or groundwater. The processes of dispersion and sorption merely dilute contaminant concentrations. Degradation removes contaminant mass from the system, thus it is the process of primary interest. It is often not difficult to demonstrate that degradation processes are occurring at a site, but it is difficult to determine if the rate of the processes will proceed at a pace to prevent harm to the environment and human health (Azadpour-Keeley et. al., 2001). MNA is widely used as a treatment solution for hydrocarbon (BTEX) plumes, but chlorinated organic solvents are often not remediated at an acceptable rate by MNA (Wiedemeier et. al., 1996). Biostimulation is a method similar to MNA, except that electron donors, electron acceptors, and/or nutrients are added to an aquifer to stimulate microbial growth. As a result, the rate of contaminant degradation is increased significantly and the contaminants are transformed faster than would be if the microbes were not stimulated. The method proved successful at site 19, the Edwards Air Force Base in California (McCarty et. al., 1998). A plume of TCE with concentrations ranging from 500-1200 ppb was treated with injection of toluene as an electron donor and oxygen as an electron acceptor. TCE concentrations in groundwater leaving the site were reduced by approximately 97-98% (McCarty et. al., 1998). The study was conducted in an aquifer that was relatively homogeneous and bounded above and below by thin aquitards. The remediation system was engineered for the specific hydrogeologic system, and therefore its application to other aquifers does not seem likely. Bioaugrnentation is a process that involves the addition of microbes and the necessary nutrients to sustain them into an aquifer. The microbes can be indigenous species that are added to increase the current populations, or non-indigenous organisms if the species present do not degrade the contaminant at a sufficient rate or produce undesirable intermediate products. A benchmark study in bioaugmentation was conducted at plume A in Schoolcraft, Michigan (Table 1 and Figure 2). The plume is composed of carbon tetrachloride (CT) with concentrations generally less than 100 ppb. The researchers designed a system to inject a CT degrading bacteria and nutrients into a zone referred to as a “biocurtain”. The biocurtain extended vertically over the entire thickness of contamination and groundwater passively moved through the treatment zone and CT was degraded. CT in plume A has been successfully remediated for over 3 years (Hyndman et. al., 2000). In addition to the bioaugmentation research currently being conducted at Schoolcraft plume A, a bioremediation system is being developed at the Schoolcraft plume G site. The main goal is to design and implement an in situ bioremediation system that will be applicable to a wide range of hydrogeological conditions and will be much more cost effective than traditional remediation methods, such as pump and treat systems. SCOPE OF WORK The research contained in this thesis was used to develop a more thorough understanding of the flow and natural attenuation processes at plume G. The primary objective was to develop a 3-D reactive transport model at the plume scale and to estimate the rates of degradation of the contaminants contained within plume G. The steps used to complete the aforementioned objective were as follows: 0 Chapter II - Construction and calibration of a 3-D, steady state, regional scale, groundwater flow model for the area surrounding the village of Schoolcraft 0 Chapter III - Construction and calibration of a 3-D, steady state, plume scale, groundwater flow model using heads derived from the regional model 0 Chapter IV - Construction and calibration of a 3-D reactive transport model of plume G using the plume scale flow model to estimate the rates of degradation of the source contaminants and their daughter byproducts The regional flow model incorporated natural hydrologic boundaries and regional scale geologic features to more fully understand the hydrogeology of the area and to determine the spatial pattern of hydraulic heads at the plume site. The plume scale flow model was constructed with a more refined grid than the regional model, which enabled inclusion of more heterogeneity to better represent contaminant transport. The hydraulic heads of the regional model were incorporated in the local model through telescopic grid refinement. The plume scale flow model served as the basis for the transport modeling activities to explore the movement and degradation of PCB, TCE, TCA, and their degradation byproducts. CHAPTER II THREE-DIMENSIONAL REGIONAL STEADY STATE GROUNDWATER FLOW MODEL OF SCHOOLCRAFT, MICHIGAN INTRODUCTION Wiedemeier et. al. (1996) strongly recommended the use of detailed groundwater flow and coupled contaminant transport models as part of the investigation of natural attenuation processes. A groundwater flow model was created as the first step in the evaluation of the degradation of chlorinated organics at plume G. While groundwater flow models can be valuable tools, they are only reliable and thus useful if all aspects of the modeling process have been critically evaluated and the natural system adequately represented. Anderson and Woessner (1992) indicated that one of the most important aspects of modeling is the appropriate choice of boundary conditions. Reilley (2001) indicated that the key in boundary selection is to choose model boundaries that correspond to features in the model system that minimize artificial approximations. Anderson and Woessner (1992) stated that the best boundaries to use are physical boundaries, such as impermeable rock units (or units that have a hydraulic conductivity that is two orders of magnitude less than the modeled unit). If physical boundaries are not readily present in the system, then hydraulic boundaries, such as regional groundwater divides, are the next best type to use (Anderson and Woessner, 1992). Physical and/or hydraulic boundaries were not immediately found in Schoolcraft on the small scale that was needed to complete a detailed analysis of natural attenuation at plume G, but past studies by Buxton and Reilley (1986), Miller and Voss (1987), and 10 Ward et. a1. (1987) outlined a method to overcome these difficulties. Simply stated, a large “regional scale” flow model with a coarse grid can be created that encompasses physical and hydraulic boundaries that are far removed from the local study site, yet control its groundwater flow. Specified head or specified flow boundaries can be interpolated from the regional model for an embedded smaller scale refined local flow model. The process is commonly referred to as “telescopic mesh refinement” (Anderson and Woessner, 1992) or “telescopic grid refinement” (BYU, 2000). Therefore, a regional scale model was built to estimate the spatial distribution of flow for a plume scale local flow model. PREVIOUS WORK The site geology, hydrogeology, and hydrology of the Schoolcraft area were assessed to develop the regional model. The bedrock is the Mississippian Coldwater Shale, which is subsequently overlain by Pleistocene glacial deposits (Martin, 1957). Investigations by Martin (1957), Dorr and Eschman (1970), Ibrahim (1970), and Lillienthal (1978) provided descriptions and maps of the Coldwater Shale. The glacial deposits were initially described and interpreted by Leverett and Taylor (1915). Subsequent work by Martin (1957), Monaghan et. al. (1986), Monaghan and Larson (1986), and Finkbeiner (1994) provided further insight into the complex glacial history of the region surrounding Schoolcraft. The hydrogeology and geochemistry of the aquifers in the region were evaluated by several authors due to agricultural and industrial contamination (Barrese, 1991; Steinmann, 1994; Kehew et. al. 1996; Hyndman et. al., 2000). The conceptual model was based on the results of the literature review. 11 Regional Geology The bedrock underlying Kalamazoo County is mostly composed of the Coldwater Shale except for a small portion of the northeast comer of the county that is composed of the Marshall Formation (Figure 3). The Coldwater Shale was deposited as a sequence of fine-grained muds in the Early Mississippian Period of the Paleozoic Era when the region was an offshore marine environment (Dorr and Eschman, 1970). The formation is about 150 meters thick near Kalamazoo County and generally dips to the northeast (Martin, 195 7). The shale is gray to blue-gray in color, contains small amounts of limestone, dolomite, siltstone, and sandstone, and is separated from the underlying Ellsworth Shale by a 3-6 meter thick layer of red argillaceous limestone/dolomite commonly referred to as the Coldwater Redrock (Martin, 1957). Ibrahim (1970) conducted extensive geophysical mapping of the surface of the Coldwater Shale underlying Kalamazoo County, as did Forstat and Sorenson (1982). Both showed that the bedrock surface in the area of interest generally slopes in a WNW direction. The Coldwater Shale is considered to be a low conductivity hydrostratigraphic unit and aquifers are subsequently only found in the overlying glacial sediments (Kehew et. al., 1996). The Marshall Formation was not examined since it was approximately 40 km from Schoolcraft and was not in the model area. Kalamazoo County’s bedrock is overlain by thick deposits of glacial sediments (Leverett and Taylor, 1915). The western three-quarters of the county are sediments deposited by the Lake Michigan Lobe of the Laurentide Ice Sheet, while the eastern quarter of the county is underlain by deposits of the Saginaw Lobe of the Laurentide Ice Sheet (Figure 4) (Leverett and Taylor, 1915). A surficial geologic map modified by 12 .IDCK GEOUXIY OF [OWE]! PHINSUIA m Bans mum ERMA‘I'DN snormw rem-mu - MYPOIII' UMBS'IDNE - mute»: FORMATION - mm romxmn - comma: SHAH! smaunv sum: mum s; a man at - IDPORD sum uswormr SHALE m SHALE mvm snow mu. smut mm mansion: - canon mm mow - mm mrommn - uss numcnouv - sum mom KALAMAZOO COUNTY km >2 Figure 3. Bedrock map of the Lower Peninsula of Michigan with Kalamazoo County enlarged (modified from Milstein, 1987). Note that the Coldwater Shale is Chartreuse, while the Marshall Formation is gray. Image is presented in color. Z V: E9 E.) 5' Lu M <1: ..I é ’ / . $05“ / l‘ .’ . 2'” dz “Prams // [DA 2% \AM /!5 . . \C%@ I'/ . \ / \ \ .\ + drumlin I W A, 4“ {27 county lines ’ I / 6,, ‘V a _._.interlobate e°~ , boundary r / / l’ G“ {3“ \ // 0 15 \ ._____. 0 as} 43 km 0 Schoolcraft MICHIGAN LOBE MORAINES SAGINAW LOBE MORAINES LBM - Lake Border Moraine TkM - Tekonsha Moraine IVM - Inner Valpraiso Moraine KM - Kalamazoo Moraine OVM - Outer Valpraiso Moraine ChM - Charlotte Moraine IKM - Inner Kalamazoo Moraine LaM - Lansing Moraine IKM - Outer Kalamazoo Moraine StM - Sturgis Moraine TkM - Tekonsha Moraine Figure 4. Map of moraines in southwest Michigan and the study area of Monaghan et. al. (1986). Note the location of the interlobate boundary that separates deposits of the Michigan Lobe from deposits of the Saginaw Lobe (modified from Monaghan et. al., 1986). 14 Rheaume (1990) from Monaghan and Larson (1982) for the county is provided in Figure 5. The surficial geology is generally characterized by outwash plains of sands and gravels lying between northeast-southwest trending moraines of undifferentiated till (Monaghan and Larson, 1982). Schoolcraft lies within the Galesburg-Vicksburg Outwash Plain. The complex glacial stratigraphy in southwestern Michigan was studied by Monaghan et. al. (1986). The authors correlated three till sheets to moraines from the Michigan Lobe of the Laurentide Ice Sheet. Figure 4 outlines the study area of Monaghan et. al. (1986) depicting the moraines of interest, the interlobate boundary that separates deposits of the Michigan and Saginaw Lobe, and the location of Schoolcraft. The till sheets were correlated based on clay mineral analyses of samples from moraines, till plains, and multi-till exposures. The authors determined that the Outer Kalamazoo Moraine of the Michigan Lobe was composed of the Saugutuk Till, while the Tekonsha Moraine of the Michigan Lobe was composed of the Ganges Till (Figure 6) (Monaghan et. al., 1986). No attempt was made to correlate the Glen Shores till inland or speculate on its stratigraphic significance since it was not seen at any other site in the area. The till stratigraphy was important since Schoolcraft is located between the Outer Kalamazoo Moraine and the Tekonsha Moraine, thus the Ganges till was expected to lie beneath the village. Finkbeiner (1994) conducted an extensive investigation of the subsurface glacial geology between the Tekonsha and Kalamazoo Moraines in Kalamazoo County (Figure 7). F inkbeiner (1994) concluded that three till units existed in the area, informally named till 1, till II, and till III, based on cross-sections constructed from water well logs and several wells drilled and logged by individuals at Western Michigan University. Till I 15 I Schoolcraft A Galesburg-Vicksburg outwash plain-Mostly medium to very coarse sand and gravel. Pebble to cobble gravel common. Climax-Scotts outwash plain-Mostly medium to very coarse sand and gravel. Pebble to cobble gravel common. Downcut glacial drainage channel-Mostly medium to very coarse sand and gravel. Deposits from a deeply incised valley train system. Upland moraine, kame field, or highly collapsed outwash-Mostly sandy till. Boulders and cobbles common on the surface. Till plain-Mostly coarse sandy and cobbly till. Clay-rich in areas. Boulders common on the surface Figure 5. Surficial map of Kalamazoo County (modified from Monaghan and Larson (1982) in Rheaume (1990)). Image is presented in color. 16 w . . , E b" 8" é o 0° s s o o O ‘bo Q70 ‘5" A?” ‘9’ 5‘9, :9 e s s s’ e e «i .y 2’ f: A .5” 2’ e” e? 0 £4 0 £2 0 <9 0 <5“ 0° ¢° 0° x5“ 0° 03$ «£3: a SAUGATUCK TILL E .2 2 435 GANGES “LL 15 A S O STILL (I) l GLENN km Figure 6. Michigan Lobe tills correllated to respective moraine(s) in southwest Michigan (modified from Monaghan et. al., 1986). Schoolcraft lies between the Outer Kalamazoo Moraine and the Tekonsha Moraine of the Michigan Lobe. l7 e: *E‘ ". -'. N 0 ° ° ‘° 0 o .' ° C) o . '. t: o o o . . 23 :1 .° ' ° :3 . o 0 o. _ m g 1. ‘ 0 o o 5 '26 .' >4 M -' r ‘r- --- - x- 0.. \ o: ‘ \ \ \ J :° \ \ 1 l 5 I ) 3 l / 3 ‘ I : \ / . _ . ‘ / ,2." / \ I, ’3' Schoolcraft ) o I .- J f 53' l” K\ ~ Kalamazoo County ' ‘~ ~. “ ‘ St. Joseph Countyl \ \ _J ~ I_ _ _— 0 8 --- Boundary of F inkbeiner’s Study Area . km ' — Trace of the Tekonsha Moraine - ° - 0 Outer Kalamazoo Moraine Figure 7. Map showing the approximate boundary of the Finkbeiner (1994) study area (modified from Finkeiner, 1994). Note the trace of the Tekonsha Moraine, which is discussed in the text. 18 was areally extensive and found to lie directly above bedrock. F inkbeiner (1994) interpreted that till I may be pre-Wisconsinan in age based on research conducted on an apparent paleosol (possible Sangamon Paleosol) above till I by Passero (1981). Till H was located above a layer of outwash that was deposited on till I and is areally extensive; however till H is missing west of Schoolcraft. Till III was a discontinuous diamicton layer that was deposited above another layer of outwash that covers till 11 and was only seen in the northern half of the study area, about 6 kilometers north of Schoolcraft (Finkbeiner, 1994). Leverett and Taylor (1915) originally hypothesized that the Tekonsha moraine may have been buried in southeastern part of Finkeiner’s study area and the author also delineated and interpreted an unnamed till as being a buried arm of the Tekonsha moraine (Figure 7). Kehew et. al. (1996) reiterated that this buried till sheet may be either a buried extension of the Tekonsha moraine, a buried margin of a drumlinized till sheet, or a combination of both. The tills were never interpreted in the context of the tills identified by Monaghan et. al. (1986). Review of both studies suggests that F inkbeiner’s (1994) till II corresponds to the Ganges Till of Monaghan eta]. (1986). Regional Hydrogeology The hydrogeology and geochemistry of the aquifer underlying Schoolcraft were investigated by Barrese (1991), Steinmann (1994), and the subsequent results were presented by Kehew et. al. (1996). A discrete glaciofluvial deposit named the Prairie Ronde Fan that encompasses the Schoolcraft area was identified (Figure 8). The fan was delineated based on topographic and geomorphic criteria. It is composed of sands and gravels deposited by meltwaters of the stagnant ice margin that formed the Kalamazoo 19 2.- ? '. '. 5 N a :3 .0 o. . . 8 . - - '~- A U U : .0 c: 8 ' ° 2 N °' ° ' 3 cc . . __ 5 § ,. -."n ~- 51. E .-' 3.... /I .~.' I". Kalamazoo County ‘ St. Joseph County 0 g I: Prairie Ronde Fan ' I _ Trace of the Tekonsha Moraine km ' ' ° ‘ Outer Kalamazoo Moraine Figure 8. Location of the Prairie Ronde Fan presented by Steinmann (1994) (modified from Kehew et. al., 1996). 20 Moraine of the Michigan Lobe. Kehew et. al. (1996) notes that there are scarps in the Kalamazoo Moraine that mark the partially collapsed channel that served as the outlet for meltwaters that created the fan. The sediments are thickest near the Kalamazoo Moraine and thin as one moves east-southeastward until it terminates against the margin of the buried till sheet described by Finkbeiner (1994) and Kehew et. al. (1996). The aquifer in the Prairie Ronde Fan was studied by construction of water table contour maps, geochemical analyses, and through slug tests. Steinmann (1994) showed that the recharge area for the aquifer was the topographically high area of the Kalamazoo Moraine and that the discharge area for the aquifer was the Howard-Barton chain of lakes to the southeast of Schoolcraft (Figure 9). Barrese (1991) determined from tritium studies that flow within the aquifer was stratified. The author identified an upper flow system that interacted with the ponds and wetlands in the area, and a deeper flow system that did not interact with the surface waters until it discharged at the Howard-Barton Lake system. Even though both systems were somewhat separated, both displayed properties of unconfined aquifers indicating that there was no laterally extensive confining unit present in the system. Steinmann (1994) also stated that in general, the outwash in the lower aquifer was composed mostly of medium grained sands, while the upper aquifer was composed of coarser grained sands. Slug tests in the aquifer indicated that conductivities in the outwash were on the order of 10'2 cm/s. Regional Hydrology Rheaume (1990) investigated the regional hydrology of Kalamazoo County. The author outlined three major drainage basins, which were the St. Joseph River basin, the 21 Paw Paw River basin, and the Kalamazoo River basin. Schoolcrafi lies in the St. Joseph River basin. Several surface water bodies occur near the village: Sugarloaf and Gourdneck Lakes to the north, Sunset Lake to the east, the Howard-Barton lake system to the southeast, Spring Creek to the southeast, and F lowerfield Creek to the southwest (Figure 9). Several wetlands also exist in the area, most notably are Kramer Marsh, Harrison Lake, and Schug pond, all to the northwest of the village (Figure 9). The Kalamazoo Moraine to the northwest of Schoolcraft provides a significant topographic divide, and the groundwater divide has been shown to closely mimic this surface water divide (Figure 9) (Rheaume, 1990). Rheaume calculated groundwater recharge from precipitation for the county to be 23.7 cm/yr based on the method of baseflow separation described in Freeze and Cherry (1979). CONCEPTUAL MODEL The regional model was developed using the conceptual model approach (Bear et. al, 1992; Anderson and Woessner 1992). The boundaries and model layers were conceptualized based on the results of the intensive literature review of previous investigations of the geology, hydrogeology, and hydrology of Schoolcraft. The numerical model was based on the conceptual model described below. Conceptual Boundaries Choosing the model boundaries was a critical step in the flow model design since the flow pattern is heavily determined by the boundary conditions (Anderson and Woessner, 1992). Starting to the north of Schoolcraft and moving in a clockwise 22 \ / - 4/ Sunset Lake L l / K K Portage Creek Mud Lake ~—-‘ A \ Howard Lake Harrison Lake 0 All?" ' __ r Barton Lake Schug Pond " l Schoolcrafi ‘ '\ Spring Creek F lowerfield Creek /\/ Roads N Rivers/Stream W/A Moraine I "x ’ Drain a Wetland Lake 0 4 2 km Figure 9. Location of the significant surface water bodies in the vicinity of Schoolcraft, Michigan that served as boundaries in the regional model. The perimeter boundaries that are not hydrologic boundaries are no flow boundaries interpreted as topographic divides from the DEM. 23 direction, the following were chosen as natural hydrologic boundaries: Sugarloaf Lake, Gourdneck Creek, Gourdneck Lake, Sunset Lake, Barton Lake, Howard Lake, Spring Creek, Flowerfield Creek, and the Kalamazoo Moraine (Figure 9). Natural hydrologic boundaries were defined at surface water bodies that were shown to be locations of groundwater discharge (Steinmann, 1994; Rheaume, 1990) and along the Kalamazoo moraine, which was shown to be a groundwater divide (Rheaume, 1990; Steinmann, 1994). Gaps that existed between these boundaries were filled by interpreting topographic highs that were likely no flow boundaries. Several wetlands occur within the model area that were shown to play a significant role in the movement of groundwater in the unconfined aquifer by Steinmann (1994) through examination of water table maps of the aquifer. These were also represented as hydraulic boundaries in the model. Conceptual Layers The previous studies that were completed in the region provided sufficient information to determine the number of layers needed to describe the model area. Based on the investigations conducted by Barrese (1991), Steinmann (1994), F inkbeiner (1994), and Kehew et. al. (1996), the region can be separated into three main layers in the vertical plane (Figure 10). The base of the model was the top of the till sheet that lies on the Coldwater Shale that was described and informally named as till I by Finkbeiner (1994) and presented in Kehew et. al. (1996). The till was described as being predominantly clayey and thus provided a good barrier to downward flow. Kehew et. al. (1996) indicated that the till layer may not cover the bedrock over the entire region, but in any case, the Coldwater Shale lies directly below the till and would also serve as a barrier 24 to water flow in the absence of the till unit. The entire bottom layer was modeled as a layer of outwash. It was unreasonable to think that these deposits were homogeneous, but no other data were available to further delineate the zone. The middle layer coincided with the layer of till that occurs approximately 27 meters below the Village of Schoolcraft and acts to retard the downward migration of plumes A-G, which corresponds to Finkbeiner’s (1994) till H. The till was not found in the entire region, especially in the middle of the model area where outwash was present. The deposits of the middle layer were delineated later during an investigation of the water well logs in the region. The top layer extended to the ground surface and was predominantly outwash deposits except for the sediments of the Kalamazoo Moraine to the northwest of Schoolcraft. The outwash deposits of the top and middle layer were modeled as being slightly coarser and thus more conductive than the outwash found in the bottom layer based on well log descriptions and slug tests presented in Steinmann (1994). The conceptual model was the most important step taken when the regional model was developed. The boundaries were carefully chosen based on the results of the literature review. The model layers were determined from the literature review as well. The data was assimilated and summarized to help ensure accuracy of the model construction. A flow chart that presents the relevant results of the conceptualization process is depicted in Figure 11. 25 3.8 E voEomoa mm owns: 3805—25 cobw— 338 38038 8: cc 830535 Hob: onE .388 3:032 06 0533388 9 wow: fine—Snow wage—am .328» Ecomwoc 05 mo 8308-390 Banana .3 0.5mm." Beau 22m Leeaaeo I see any: .38“ 2 3:85 r eséeo 3608 05 . E 32 2.. E 8E5 I E5 _E .033 I segue as. ass 3.82 I said I Eamoa on .38 man—o 05.332 33:32 I .5. was» as... 382 r _E 22:2 25 Beam i gees: 85.8.3 I % MM\ EH a £3380 3:30 I Sa— H v c exam >\ 0:502 E .\\\\\\x 530 338 I N MES 32 IMPLEMENTATION OF THE CONCEPTUAL MODEL The conceptual model was implemented as a steady state finite difference groundwater flow model. The USGS code MODFLOW (McDonald and Harbaugh, 1988) was used to solve the 3-D steady state saturated groundwater flow equation. The Groundwater Modeling System (GMS) (BYU, 2000) preprocessor program was used to create the necessary input files for MODFLOW and to visualize the results. Development of the model in GMS consisted of several steps. In general, the process was to build a 3-D grid based on GIS data, interpolate the layer elevations from well log data using geostatistical methods, assign model boundaries using previously delineated GIS data, and calibrate the model to field data. Calibration was achieved through a simple trial and error process of manipulating conductivity values until an acceptable match was obtained between simulated and observed head values. Development of a 3-D Finite Difference Grid A 3-D finite difference grid was developed in GMS for the regional scale model. The DEM was imported as a 2-D grid into GMS and a 3-D grid was then constructed so that the model boundaries previously defined in ArcView fit within. The grid was 611 cells by 645 cells by 3 layers in the X (East) and Y (North) and Z (vertical) directions respectively. The cells were 30 m by 30 m in the horizontal plane but variable in thickness in the vertical plane. The DEM elevations were then interpolated to the 3-D grid as the top elevation of the model. The grid was oriented in a manner such that the MODF LOW cells directly coincided with the cells of the DEM to insure direct interpolation of the DEM values. The ArcView polygon that represented the model 33 boundaries was then imported into GMS and the cells within the polygon were activated. The model was then split into three layers in preparation for geostatistical interpolation of the model layer bottom elevations. Layer Elevation Interpolation The layer elevations were interpolated using 2-D geostatistical methods in GMS. The layer elevations were more difficult to interpolate for the lower layers than the top layer because there were fewer wells penetrating the deeper sediments; therefore, less data were available to use in the interpolation process. The number of sample points representing layer elevations decreased from layer 1 to layer 2 and layer 2 to layer 3. For layer 1, 47 wells were identified that showed the contact between the bottom of layer 1 and the top of layer 2. Many of these points, approximately 25%, were within the limits of the plume scale model, which is described in Chapter H1. The elevations were interpolated using ordinary kriging in GMS with a spherical model having an isotropic range of 6700 m and a variance of 35 (Figure 14). For layer 2, only 37 wells were identified that showed the contact between the bottom of layer 2 and the top of layer 3. The elevations were also interpolated using ordinary kriging in GMS with an exponential model having an isotropic range of 6700 m and a variance of 136 (Figure 15). Lastly, the top of the till representing the bottom of the model was only found in 11 wells since very few wells penetrated to these depths (60-90 m). Therefore, a different algorithm was chosen as the interpolation scheme because a reasonable variogram could not be developed for kriging. The bottom elevations of layer 3 were interpolated using the Inverse Distance Weighted algorithm in GMS. The final model interpolated 34 layer elevations are depicted in Figure 16. Model Boundary Assignment The boundaries that were identified in the conceptual model were applied to the numerical model. The surface of the top layer was a recharge boundary upon which a value of 23.7 cm/year of recharge was assigned (Rheaume, 1990). The base of the model was represented as a no flow boundary since it was the top of a till layer. The streams and lakes were assigned as constant head boundaries in all three layers. The value of head in each lake cell was equal to the value of the DEM, which was checked against the most recent topographic map to ensure accuracy. The value of head that was assigned to each stream constant head cell was a value equal to the DEM minus 0.6 m (2 ft). The stream constant head values were lowered because the streams were smaller than the 30 m DEM cells, and therefore a stream that is downcut through an area would have an elevation lower than the averaged elevation that was assigned to the DEM cell. . The wetlands were designated as general head boundaries in the top layer only. The justification was based on research presented in Kehew et. a1. (1996) that showed that the wetlands in the area typically only affected the local flow system and not the deeper regional systems. The F ollmer drain is located to the east of Schoolcraft and it was assigned as a drain boundary in the top layer of the model. All of the aforementioned boundaries were applied to the model through the map module of GMS with coverages that were created in ArcView. Hydraulic Conductivity Assignment Several conductivity zones were identified in the model area (Figure 13) and 35 6O { O.) .2 a: 2% 40-- Eb -:: 20*- a: > 0 2000 4000 6000 Lag Distance (m) Figure 14. Variogram for interpolation of layer 1 bottom elevations. 150" .. 100“ 50‘" Variogram Value 0 ' 2000 ' 4000 6000 Lag Distance (m) Figure 15. Variogram for interpolation of layer 2 bottom elevations. 36 Elevation (m) Layer 1 ‘ Data Point Elevation (111) - Layer 3 ‘ Data Point Figure 16. Interpolated model layer bottom elevations. The location of the data points from which elevations were interpolated are shown as triangles. 37 these parameters were applied to the model. Initially, representative conductivity values for the different aquifers materials were assimilated from a variety of sources, most notable were Mayotte (1991), Kehew et. al. (1996), and Hyndman et. al (2000). The conductivities were assigned using coverages created in ArcView (Figure 13) that were mapped to MODF LOW using the MAP to MODFLOW command of the map module of GMS. Assigning conductivities in this manner allowed for easy manipulation of values during the calibration process. MODEL CALIBRATION The regional model was calibrated to ensure that the model reasonably represented the natural flow system. A data set that was specific to the plume site was used to compare model results. The model conductivities were varied and the simulated head data were analyzed until a reasonable match was obtained with the observed data. The objective function was to minimize the root mean squared error (RMSE) of simulated vs. observed heads. Observed Head Data Set The observed head data that were available for this project consisted of a set of approximately 50 observations made in monitoring wells in and adjacent to the village of Schoolcrafi. The data were collected June 23—27, 1989 by the NUS corporation during their RI/FS study of plumes A and F. Additional data were available in the form of static water levels from the water wells in the area that were recorded when they were installed. The water well data may not be very reliable since they were recorded over a broad time 38 span and consequently a wide range of climatic conditions. In addition, the head readings were recorded immediately after the wells were drilled and installed, therefore, the aquifer was disturbed and head readings may be inaccurate. The calibration process consisted of matching the simulated heads to the NUS data, while using the regional data set to check that the general trend of simulated vs. observed values over the entire model region was reasonable. Only the static water level data from wells that were surveyed to +/- 1 meter of the DEM elevation were included in the regional data set. Results The steady state groundwater flow model was calibrated to minimize the RMSE between the simulated and observed heads. This was achieved by adjusting the four different hydraulic conductivity zones until a reasonable match was achieved. The final conductivity values compare well with values determined by slug tests in the region presented in Kehew et. al. (1996) (Table 2). The simulated heads are plotted relative to the observed heads (Figure 17), which shows that the model reasonably predicts the observed heads since values were within +/- 0.15m and the RMSE was 0.003 m. The simulated regional heads also compared reasonably to the to the large database of heads taken when the water wells were drilled, however the reliability of this data is subject to question as discussed previously and a plot is not presented. A plot of the calibrated head distribution for the top layer of the model is given in Figure 18 Discussion The head map with superimposed flow vectors (Figure 19) shows that flow is 39 263 262.5 *' Computed Head (m) 261 — ---------------- 1-0-. ------------- ----------------- ---------------- ---------------- a 262 ,_ ................ ............. :. ................. : ................. :, ................ ._ 2615 _ ................ ....... . ......... ................. ................. ', ......... 261.5 Observed Head (m) 40 Figure 17. Simulated vs. observed heads for the observation wells in the vicinity of Schoolcraft. >2 ‘ I ll l‘ l‘ ill "il‘llllillliil'mi‘i1 i illii il “in“ I “ lillllm i fl H l llllll "W llllllllllllllll "N i ii i \lllllllliil “hi liliih ' “llllllll lillliliiliililil y Mil“ llllllll lllllllll ll Heads (m) Boundary Key I 272-276 I “\ ’ No Flow m 268-272 264-268 N Constant Head 260'264 “WWW Constant Head 256-260 0 4 252456 E % General Head 248-252 km Drain Figure 18. Head distribution of the calibrated regional model (view is of the top layer). 41 generally in a southeasterly direction, but localized variations in the flow pattern exist near surface water features. Groundwater is discharging at streams and lakes, and the wetlands are providing recharge to the system. The gradient of the water table is relatively low, approximately 0.0012 near Schoolcraft. The shallow gradient was expected since the topography surrounding Schoolcraft is very flat. Examination of Figure 19 also shows that if plumes F and G were to continue to move downgradient, they may eventually reach Barton Lake. Table 2. Hydraulic conductivities of the various materials in the regional model. Material Model K (cm/s) K (cm/s)l K (cm/s)2 coarse outwash 6.6 e-2 2.9 e-2 - 5.7 e-2 2.7 e-2 medium outwash 5.5 e-2 NA NA moraine 3.0 e-4 NA NA sandy till 1.0 e-5 NA NA 1. From Kehew et. al ., 1996 2. From Hyndman et. al ., 2000 Two minor difficulties arose during the model calibration process that affected the model results. When the model was first constructed, the DEM elevations were assigned as the elevations of the stream constant head boundaries. The simulated heads were approximately 0.6 m (2ft) too high for this scenario. The conductivity values were increased in order to lower the modeled heads, but even at unreasonable values (10 cm/s in the coarse outwash), the heads were still too high. The model was reevaluated and it was determined that streams in the model area were not 30 m wide, and therefore spatial averaging of the DEM likely increased the elevations of cells where streams existed. The stream constant head elevations were subsequently lowered by 0.6 m, which fit well with 42 >2 l'lll' 7 ll" | .. ‘ ..Il . j .‘l ‘ I 1 w l ,. ll||||| [/— . R .. | ~ - .Ill”ill A r 4 {lll'illiilk . |. lilll ' Heads (m) Boundary Key I 272-276 .. , .. I. 268-272 ’ ‘ N°F1°W llllllll 264-268 Constant Head 260-264 llllllllllllllllll Constant Head 256-260 0 4 252—256 E E General Head 248'252 km Drain Figure 19. Head distribution of the calibrated regional model with flow vectors to show direction of groundwater movement predicted by the model (view is of the top layer). 43 the calibrated conductivities. Lowering the stream cell elevations by a smaller value resulted in conductivities that were much higher than the observed values, and lowering the elevations by a larger value resulted in conductivities that were somewhat lower than the observed values. Also, the wetlands located to the southwest of Schoolcraft were shown to play a significant role in controlling the head distribution. Initial model results predicted gradients near the wetlands that were too steep, as if they were not providing enough recharge. As a result, the conductance of the wetlands was increased to provide more influence from the wetlands, and the predicted gradients were much more reasonable. 44 CHAPTER III THREE-DIMENSIONAL PLUME SCALE STEADY STATE GROUNDWATER FLOW MODEL OF SCHOOLCRAFI‘ MICHIGAN INTRODUCTION A local plume scale flow model was developed to better represent the highly heterogeneous outwash deposits containing plumes A-G but was linked to the natural hydrologic boundaries through the regional model (Figure 20). The stages of the model development were somewhat similar to that used in Chapter II. A conceptual model of the heterogeneity in the aquifer was developed using numerous well logs. The conceptual model was then implemented in MODFLOW using several modules of GMS. The conductivity values for the various aquifer materials were adjusted until a reasonable match was made between the simulated and observed data. CONCEPTUAL MODEL The conceptual model approach was used to develop the local model. First, the model domain within the regional model was identified. The regional heads were then evaluated to determine an appropriate method to apply the regionally derived boundaries. Lastly, the aquifer materials were characterized so that they could be incorporated into the model. The conceptual model was the basis for the numerical model. Conceptual Boundaries The regional geology that was outlined in Chapter II was examined to determine the extent of the plume scale flow model. The three-layer regional model extended from 45 the ground surface to the till layer above the Coldwater Shale. The bottom two layers of the regional model were not incorporated into the local model because the discontinuous till unit that served as layer 2 of the regional model was continuous in Schoolcraft. The till layer was a barrier to downward flow and thus was the bottom of the local model (Figure 21A), while the ground served as the top of the model (Figure 21B). The regional heads near Schoolcraft were evaluated to determine an appropriate method to include the regional boundaries in the plume scale flow model. A common method to identify a local model based on regional flow patterns is to define stream tubes within the flow domain of the regional model. The stream tubes represent no flow boundaries on the sides of the model that are parallel to flow. The upgradient and downgradient sides of the model that are perpendicular to flow are then assigned as constant head boundaries, where each typically coincides with an equipotential line. This method was not easily implemented for Schoolcraft since the flow paths were irregular due to the numerous wetlands near the village. Instead, a more appropriate method was to define all boundaries of the local model as constant head. The process acted to embed the local model within the regional model preserving the complex head distribution. Conceptual Aquifer Material Types Several well logs were examined and interpreted to identify the nature of the outwash deposits that comprise the aquifer. A series of nine wells were drilled in a field downgradient of the ARCO facility that are a part of a test grid to conduct in situ experiments by MSU. The wells were drilled using a hollow stem auger and the core was taken using a Waterloo continuous cohesionless sand sampler. The cores were visually 46 inspected to differentiate the various grain sizes of the outwash (Appendix A). In addition to the nine MSU wells, over 100 well logs were previously collected during several subsurface investigations by the NUS Corporation during the initial stages of the RI/FS studies conducted in the late 1980’s (Figure 20). The NUS well logs are available in Mayotte (1991) and show that the wells were drilled no deeper than a few centimeters into the till layer that is approximately 27 meters below ground surface. The general trend of the sediments was cycles of fining upward sequences of gravels and coarse sands to medium and fine sands. This observation fits the previous interpretations that the deposits were the result of a system of braided streams emanating from the meltwaters of the Michigan Lobe of the Laurentide Ice Sheet (Kehew et. al., 1996). Distinct laterally continuous layers on the scale of the local model were not identifiable because of the nature of braided stream deposits. After examining the well logs, it was determined that the deposits could be represented by five different material types, a qualitative description of which is listed in Table 3. Table 3. Qualitative description of the materials comprising the aquifer in the plume scale model domain. Material General Description 1 very fine to fine sands, subrounded, medium sphericity, well sorted 2 fine to medium sands, rounded, meduim sphericity, well sorted 3 coarse sands, subangular, medium sphericity, poorly sorted 4 medium to coarse sands, some fine gravel, subangular to subrounded, low sphericity, poorly sorted 5 coarse sands, gravels, and pebbles, subangular to subrounded, medium sphericity, poorly sorted 47 LEGEND 4 NUS Monitoring Well I MSU Monitoring Well 0 500 SE Figure 20. Location and orientation of the plume scale model in reference to the regional model (cells are not shown as they are too small to be seen at the current scale). Well locations are given for NUS and MSU wells where lithologic data were available for aquifer characterization. 48 Elevation (m) 240 .5 240 .0 239 .5 239 .0 i-i 238 .5 — 238 .0 — 23?.5 23? .0 Elevation (m) 287.5 287.0 288.5 .; ,. 288.0 ‘ 285.5 285.0 284.5 284.0 283.5 283.0 282.5 ‘lllllllllllllllllilllillli ulliii ‘ I lll hi‘lliii lllll!’ B Figure 21. A) Contour map of the bottom of the plume scale flow model, which is also the bottom of layer lin the regional model. B) Contour map of the ground elevations in the plume scale flow model. The contour interval is 0.5 m. 49 IMPLEMENTATION OF THE CONCEPTUAL MODEL The plumes scale steady state model was created for MODFLOW through GMS. The complex stratigraphy was incorporated by using the Borehole, TIN, and Solid modules of GMS. Telescopic grid refinement was performed as a regional to local conversion in GMS to embed the local heads within the regional model. The local model was calibrated with the same head data as the regional model. Development of a 3-D Finite Difference Grid A 3-D finite difference grid was created in GMS that represented the plume scale flow model. Several factors were considered before the grid was built including the extent of plume G, the location of the wetlands near the village, and the appropriate vertical discretization to adequately incorporate the aquifer heterogeneity. After these factors were considered, a 3-D finite difference grid was created and the physical attributes are given in Table 4. The grid was rotated in the X/Y plane 47 degrees in a counterclockwise direction to align its long axis roughly parallel to groundwater flow. Also, it should be noted that the cells of the local model were 10 m by 10 m (in the horizontal plane), which was scaled down from 30 m by 30 m in the regional model. The location of the local model in reference to the regional model is shown in Figure 20 along with the locations of boreholes that were used to conceptualize the aquifer materials. Table 4. Physical characteristics of the plume scale groundwater flow model (all cells were active). Direction length (m) length (ft) # cells cell size (111) cell size (ft) X 1200 3937 120 10 32.81 Y 2300 7546 230 10 32.81 Z variable variable 10 variable variable 50 Creation of Aquifer Solid Materials in GMS Three-dimensional solid objects that represented the aquifer materials described in Table 3 were used to incorporate the aquifer heterogeneity into the plume scale model. The borehole data from the MSU (Appendix A) and the NUS (Mayotte, 1991) wells were imported into GMS. Triangular interpolated networks (TIN ’s) were created from the boreholes that represented the different aquifer materials. Solid objects were created from the TIN ’s and were assigned hydraulic conductivities. The conductivity values that were given to each material were obtained from slug tests conducted by the NUS Corporation during the RI/FS of plumes A and F (the well screens were between 1-2 m long in each well and were then correlated to the different aquifer materials). The slug test data were interpreted using the method of Bouwer and Rice (1976) (Mayotte, 1991). The initial value that was assigned was the average value determined for each material. The resulting solids were the basis for the various layers of the MODF LOW finite difference grid. Several cross-sections through the solids, two parallel and two perpendicular to groundwater flow, are given in Figure 22 that represent the aquifer materials in the local model. A more detailed description of the solid stratigraphy modeling is provided in Appendix B. Interpolation of Aquifer Solids to the MODFLOW Grid The aquifer heterogeneity was applied to the MODF LOW grid using a mapping function in GMS that interpolates layer elevations and assigns material properties to cells in the MODFLOW grid based on the 3-D solids. Three mapping algorithms exist in GMS and each could have potentially yielded different results. The three methods of 51 interpolation are referred to as Boundary Matching, Grid Overlay, and Grid Overlay with Keq by GMS (BYU, 2000). The Boundary Matching algorithm creates layers that strictly match the stratigraphic layers defined by the solids while also maintaining continuous layers as per MODF LOW requirements. The major disadvantage of this interpolation scheme is that thin layers are often created where stratigraphic units pinch out, which will cause convergence problems in MODF LOW and subsequent transport simulations, thus this method was not used. The Grid Overlay method creates layers that are relatively uniform in thickness at a given X/Y location. The material properties are assigned based on which solid encompasses the center of the grid cell. The Grid Overlay with Keq option is identical to the Grid Overlay method in terms of how the layer elevations are assigned, except that the conductivities in cells where multiple materials are present are calculated differently. GMS uses an algorithm that computes equivalent horizontal and vertical conductivities based on the volume of each material in the cell. Figure 23 provides a visual representation of the three different interpolation methods for an arbitrary model (BYU, 2000). A final consideration that was given before the solid materials were mapped to the grid was that it would be unnecessary to discretize the materials above the water table as MODFLOW only describes the saturated portion of the aquifer. Inactive cells would result if multiple layers existed above the water table, but the problem was easily circumvented. Examination of the well logs revealed that the material above the water table was a relatively homogeneous unit of fine sand. There probably was more heterogeneity in this zone, but it was not identified in the well logs. Subsequently, the solids above the water table were truncated so that GMS would not discretize the 52 I LEGEND I D Material 1 — Very Fine to Fine Sand - Material 2 — Fine to Medium Sands - Material 3 — Coarse Sands - Material 4 — Medium to Coarse Sands some Gravel - Material 5 — Coarse Sands, Gravels, and Pebbles ————— Location of Cross-Sections A NUS Monitoring Well MSU Monitoring Well Figure 22. Selected cross-sections through the 3-D GMS solids that represent the aquifer materials in the plume scale model. The locations of the wells used to create the solids are given on the inset. Image is presented in color (VB = 20X). 53 D Figure 23. Graphical depiction of the results of the three GMS algorithms to map solid material properties to a hypothetical MODFLOW model. A) An arbitrary set of solids. B) Cross-section through A) using Boundary Overlay. C) Cross-section through A) using Grid Overlay. D) Plan view of layer in A) showing the smoothing effects of Grid Overlay with Kwq (modified from BYU, 2000). Image is presented in color. 54 materials above it. The DEM elevations were interpolated back to the local grid alter the material properties and layer elevations were assigned from the solids to correct the ground elevations. This action stretched out the top layer, while leaving vertical discretization of the lower layers unchanged. Boundary Assignment The model boundaries that were previously identified were applied to the model. The calibrated head distribution from the regional model was interpolated as the starting heads of the local model using the Inverse Distance Weighted Algorithm in GMS. The four sides of the model were then assigned as constant head boundaries. The top of the model was assigned as a recharge boundary with a value of 23.7 cm/yr that was used in the regional model. MODEL CALIBRATION Results The model was calibrated by adjusting the conductivities of the five different aquifer materials. Table 5 provides information on the conductivity data available to calibrate the local model. Listed in the table for each of the five material types are the number of values, the average K, the high K, the low K, and the final K for each material used in the model. The conductivities were constrained between the high and low conductivity values for the respective material during the calibration process. Also, during calibration it was noted that heads were mounding in the interior portions of the model, which was fixed by lowering the recharge to 12 cm/yr. The resulting calibrated 55 local model heads match the heads from the regional model (Figure 24). The simulated heads were plotted with respect to the observed heads for the regional and local models, close inspection reveals a reasonable match (Figure 25). Also, the root mean square error (RMSE) of the regional calibration was 0.003 m, while the RMSE for the local calibration was 0.006 m, which is also a reasonable match. Table 5. Hydraulic conductivity data (K) for the different aquifer materials described in Table 3 (observed data from Mayotte, 1991). Material # values ligh K (cm/s) Low K (cm/s) Avg. K (cm/s) Model K (cm/s) 1 3 4.00E-02 4.50E-03 9.30E-03 2.60E-02 2 6 5 .80E-02 6.30E-03 4.10E-02 3 .50E-02 3 5 9.00E-02 4.00E-02 5.50E-02 6.00E-02 4 1 1 7.50E-02 3.50E-02 4.60E-02 8.80E-02 5 5 1.10E-01 5.20E-02 7.10E-02 1.00E-01 Discussion The calibrated head distribution was extremely important since all transport modeling was completed using the plume scale model. Early simulations predicted the observed head values at the monitoring wells rather well, but the head pattern did not adequately match the regional distribution; the heads were too high in central area of the model. Initially, it was thought that the starting heads were interpolated incorrectly from the regional model. Inspection of contours from the regional model overlain upon the plume scale model showed that the boundaries were interpolated correctly. The next logical step was to increase hydraulic conductivity. The conductivity values were increased in all of the aquifer materials to a value equal to the highest observed values in Table 5, but the problem persisted. The aquifer materials were then assigned the 56 0 500 SE meters Head (m) 2628-2632 2624-2628 2620-2624 1' '1 261.6-262.0 “ 2612-2616 260.8-261.2 2604-2608 Figure 24. Head distribution of the top layer of the calibrated plume scale model, which shows flow is in a southeasterly direction. The local heads are shown in grayscale, while the regional heads are superimposed in black. Inspection between the two distributions reveals a reasonable match. 57 263 I I I I I I I I I I I I T I I I I I f I I I I I 262.5 e ---------------- ----------------- ----------------- ---------------- a l u v i a I . ' I ‘ ‘ u ‘ s I . ' . :26:Z ._ ................ r ............. ....' .............................. . .................. a u l , ' ' s . . I. l— ' I . ‘ . ' n . . 9 ' I u l ‘ I , . . ‘ . . n I u u I I - Computed Head (m) 261.5 — """""""" """"""" """"""""" """"""""" """""""" ‘ 261 __ _______________ €09 ____________ __________ 9 Regional Model _________ _ Q; 3 0 Local Model Observed Head (m) Figure 25. Plot of simulated vs. observed heads for the plume scale and regional scale model. 58 conductivity value of the layer 1 outwash from the regional model and simulated as homogeneous, but again the problem persisted. The recharge was reduced by 50%, and the head distribution of the plume scale model matched the regional distribution much more reasonably. If the problem had not been fixed, the subsequent transport simulations would have predicted irregular plume shapes that were spreading in a direction transverse to flow much more than what was observed. 59 CHAPTER IV THREE-DIMEN SION AL REACTIVE TRANSPORT MODEL OF PLUME G, SCHOOLCRAFT, MICHIGAN INTRODUCTION The transport and decay processes of plume G compounds emanating from ARCO industries in Schoolcraft, M1 were evaluated using a numerical model. The model was developed by analyzing past investigations of the ARCO site, reviewing literature pertaining to degradation of the source chemicals, and evaluating geochemical data to evaluate potential transformation pathways. The transport, sorption, and decay of the plume was represented using an RT3D model, which was built in GMS within the plume scale flow model described in Chapter HI. The model was calibrated using a new approach that compares calculated ratios of compounds to their daughter byproduct (termed mother/daughter ratios) for observed field data and model simulated results. The degradation rates were adjusted during the calibration process but were constrained between observed rates presented in Suarez and Rifai (1999). The model reasonably predicted mother/daughter ratios at a monitoring well transect downgradient of the ARCO facility. The calibrated degradation rates were low in comparison with the range presented in Suarez and Rifai (1999), but are on the same order of magnitude as those observed at the Dover site as reported by Clement et. al. (2000). ARCO SITE BACKGROUND The source of plume G was ARCO Industries Corporation (ARCO), located on East Eliza Street in Schoolcraft, Michigan. ARCO was an automotive parts manufacturer 6O that used chlorinated solvents to degrease parts in the production process and to clean the plant floor. The facility opened in 1953, but ARCO did not assume operations until 1967. Extensive sampling conducted in the mid 1980’s by ARCO led to a detailed description of the extent of contamination on the company’s property. Several remediation systems were implemented in the past to mitigate the damage caused to the environment. A review of the site investigations and remedial activities was used to develop a conceptual reactive transport model. Source Areas Five regions on the ARCO property were identified as possible sources of contamination based on visible inspection of the property and through discussions with plant employees (Everett, 1990) (Figure 26). Area I was a material and waste-handling site that was used throughout plant operations. Area H was an unlined pond that was used to hold drainage waste from the plant from 1953 until approximately 1965. Area III was a material and waste-handling site that was used throughout the facility’s operation. The South Seepage ponds were unlined pits used for handling wastewater from the plant after the Area H pond was closed in 1965. The Plasticizer Loading Area (PLA) was used for transferring bulk plasticizers from trucks into the building. The vadose zone in these five areas was sampled to identify and quantify the extent of contamination. Vadose zone soil sampling in the five suspected source areas was conducted numerous times from 1986-1991. Samples were taken mainly in the top 3 meters of sediments, but in some cases, samples from depths of up to 6 meters were obtained and analyzed. Area I was the most affected site where sediments were contaminated with 61 l 8 ii l 'l'C l lr\ SOUTH SEEPAGE POND Ir j! ' — 0 40 K 1 meters Figure 26. Location of the five suspected source areas on the ARCO property (modified from Everett, 1990). 62 tetrachloroethene (PCE) at up to 300,000 rig/kg, trichloroethene (TCE) at up to 1,200,000 jug/kg, and trichloroethane (TCA) at up to 14,000 pig/kg. Area H was not as heavily contaminated as Areal, but concentrations of PCB and TCE were 200 [Lg/kg in some portions of the old pond, while no TCA was detected. Area IH sediments were somewhat more contaminated than Area H with PCB and TCE concentrations at about 20,000 rig/kg and TCA concentrations at about 15000 [lg/kg. The South Seepage Pond contained a bottom sludge material that ranged in thickness from 0 to 2 m. Levels of PCB and TCE in the sludge were about 100 rig/kg, while TCA concentrations were about 20 rig/kg. A soil gas survey conducted in December of 1989 at the PLA indicated that chlorinated organics were present, but Everett (1990) stated that they were at very low levels. As a result, no further sampling was done in the PLA and it was not considered a significant source of groundwater contamination. Previous Remediation Systems Area I was the most heavily contaminated sector of the ARCO property and ARCO agreed to remediate the vadose zone sediments of Area I. A three-phase test was conducted from June of 1987 to September of 1988 to test the applicability of a soil vapor extraction (SVE) system at Areal. The Phase I system was composed of one injection and one extraction well while the Phase H and 1H systems included the Phase I wells, but also incorporated another set of injection and extraction wells. The three SVE tests removed an estimated 110 kg of chlorinated organics; approximately 70 kg were PCB, 28 kg were TCE, 8 kg were 1,2-dichloroethene (1,2-DCE), and 4 kg were TCA. Although the test showed promising results, a full-scale system was never implemented for reasons 63 that were never stated. Contaminated sludge was excavated from the South Seepage pond as the SVE system was being tested at Area 1. Approximately 115 m3 of contaminated sludge were removed from the bottom of the northeastern section of the pond in June of 1988. Another 64 m3 of sludge were removed from the remaining contaminated portions of the pond in May of 1989. The sludge materials were disposed off site during both excavation operations. The entire pond was back-filled with clean sand to match the existing grade after the excavations were completed (Everett, 1990). The remedial activities at ARCO shifted to development of a remediation system to treat the contaminated groundwater in the early 1990’s. The Michigan Department of Environmental Quality (MDEQ) initially decided to remediate plume G with a pump and treat system. The proposed system was composed of three purge wells, two of which already existed and were located roughly on the longitudinal centerline of plume F (PW-1 and PW-2), and one well that was installed (PW-3) (Figure 27). The stripping tower was located downgradient of ARCO and discharge was controlled by an NPDES permit that did not allow release of chromium or arsenic to the receiving water. The problem with the system was that PW-l and PW-2 would capture arsenic and hexavalent chromium from plume F in addition to the chlorinated organics from plume G if they were activated. PW- 3 was located far downgradient of plume F and about 300 meters in front of plume G (at its 1990 location), therefore chromium and arsenic were not an immediate problem. Subsequently, PW-l and PW-2 could not be used until an appropriate pre-treatment strategy was implemented to remove arsenic and chromium from the captured water before it was treated and discharged at the stripping tower. The pretreatment system was 64 A PW—l I PW—2 ° PW-3 m Figure 27. Location of the three purge wells that were part of the initial pump and treat system to remediate plumes F and G (modified from Mayotte, 1991). 65 never developed and PW-l and PW-2 never went online. However, PW-3 was activated on July 13, 1992 at a rate of 1090 m3/day and is still in operation. DEGRADATION PROCESSES The suspected initial contaminants of plume G were PCE, TCE, and TCA, as determined from past site investigations (Everett, 1990). Degradation byproducts of the source contaminants, such as cis-l,2-dichloroethene (cis-1,2—DCE), trans-1,2- dichloroethene (trans-1,2-DCE), 1,1-dichloroethene (1,1-DCE), vinyl chloride (VC), and 1,1-dichloroethane (1,1-DCA), were present downgradient of the source regions. The presence of the daughter by-products implies that contaminant degradation processes had occurred at the site. The literature was reviewed to understand the degradation pathways of the plume G contaminants in order to develop a model to mathematically describe the transformation processes. Contaminants are transformed through biotic or abiotic proceses in natural systems. Bouwer et al. (1981) presented the first evidence of biodegradation of chlorinated solvents. Since that research, many studies (including Vogel and McCarty, 1985; Freedman and Gosset, 1989; Semprini et. al., 1995; de Bruin et. al., 1992; Bradley and Chapelle, 1998) have examined processes that degrade chlorinated ethenes/ethanes in groundwater environments. A conceptual model for the transformation of PCB, TCE, and TCA that was the result of the aforementioned research is depicted in Figure 28. One of the main concerns addressed in Michigan State University’s bioremediation proposal to the Michigan Department of Environmental Quality was the abundance of VC at plume G (the MCL is 2 ppb). Review of the conceptual degradation pathways (Figure 28) shows 66 CCIZCCIZ PCE CClzCHCl CH3CC13 TCE TCA 5}} El 18351;}; <-- -_,. BC] '+ productsl )5 CClZCH2 CHClCHCl CH3CHC12 1,2-DCE 1,1-DCE 1,1-DCA -'i'cEi'I§£c§£1{{e1;’-+- -->E-'2'Ei'l'prs&uetsi CHClCH2 CH3CH2C1 VC CA i'éi';’§;£,211.‘c1;‘5<-- t r" CHZCH2 CH3COOH Ethene Ethanol Anaerobic Pathway {1.9116131515511051 ..... )Abiotic Pathway Figure 28. Biotic and abiotic transformations of PCB, TCE, and TCA under aerobic and anaerobic conditions (modified from McCarty, 1997; and Bedient et. al., 1999). All transformations are biotic unless indicated with a dotted arrow, which is the abiotic pathway. Heavy arrow indicates preferential reaction. 67 that VC can be formed by degradation of PCE/TCE or TCA. Therefore, literature that addressed transformation processes that lead to the production of vinyl chloride were reviewed. Abiotic Degradation Processes Abiotic transformation processes are less studied in groundwater systems because TCA is the only major chlorinated solvent that can be degraded at reasonable rate in this manner (McCarty, 1997). TCA can chemically transform into 1,1-DCE or ethanol (acetic acid) (McCarty, 1997). Several researchers determined in laboratory experiments that the preferential abiotic reaction of TCA was ethanol formation (Haag and Mill, 1988; Cline and Delfino, 1989). Both studies determined that approximately 79% of TCA transformed to ethanol and 21% transformed to 1,1-DCE. Although only one fifth of the degraded product is 1,1-DCE, the process is important because the MCL of 1,1-DCE is 7 rig/L and it can subsequently degrade to VC (McCarty, 1997). McCarty (1997) reported that when 1,1-DCE is found in groundwater that it is probably the result of the chemical transformation of TCA. Biotic Degradation Processes Contaminants are biodegraded directly or indirectly through the oxidation/reduction reaction of microbial respiration. The basic idea is that a coupled redox reaction occurs where electrons are passed from an electron donor through a complex series of biochemical reactions to an electron acceptor in order for the organism to obtain energy (Chapelle, 1993). The electron donor in microbial reactions is often 68 referred to as the primary substrate and in aquifers is usually the organic carbon that is present, such as humic or fulvic acid (Chapelle, 1993). The common electron acceptors in groundwater systems in order of decreasing energy yield are dissolved oxygen (DO), NO3', Fe(HI), Mn(IV), S047”, and CO; (Azadpour-Keeley et. al., 2001). The primary substrate is oxidized during metabolism because it loses electrons, while the electron acceptor is reduced because it gains electrons. A side product of metabolism is that enzymes and/or cofactors can be produced and are released into the surrounding medium (Chapelle, 1993). Microbial respiration and enzyme/cofactor production are an integral part of biodegradation. Microbial degradation mechanisms are divided into aerobic, anaerobic, and cometabolic processes (McCarty, 1997). Aerobic and anaerobic simply refer to whether the process occurs in the presence (aerobic) or absence (anaerobic) of oxygen. Cometabolic reactions occur when a contaminant is degraded by an enzyme or cofactor produced in microbial metabolism. Such processes have been referred to as fortuitous because the organism that produced the enzyme/cofactor derives no energetic benefits from the reaction (McCarty, 1997). Cometabolic reactions can occur in aerobic or anaerobic environments. Biotic Degradation Process: Occurrence Under Aerobic Conditions Aerobic processes are more energetically favorable to microorganisms than anaerobic processes, but are often not dominant transformation mechanisms in plumes of chlorinated hydrocarbons. PCE, TCE, and TCA do not serve as electron donors or acceptors in aerobic groundwater systems (McCarty, 1997). TCE can be cometabolically 69 degraded in aerobic environments, but PCE cannot (McCarty, 1997). Significant cometabolic degradation of TCE was only found to occur when large amounts of dissolved oxygen (DO) and electron donors (methane or phenol) were present (McCarty and Semprini, 1994). DCE and VC have the potential to be either directly oxidized or degraded cometabolically in aerobic environments with recent field evidence provided by Bradley and Chapelle (1998). TCA can be cometabolically degraded in aerobic environments, but the process is slow, while DCA can be oxidized in an aerobic system (Bedient et. al. , 1999). Biotic Degradation Processes: Occurrence Under Anaerobic Conditions The two degradation processes in anaerobic environments are reductive dechlorination and cometabolism. Reductive dechlorination occurs when the contaminant substitutes for either NO3', Fe(HI), Mn(IV), 8042', or C02 as the terminal electron acceptor (Wilson et al., 1997). For example, PCE can accept electrons produced during the metabolism of an oxidizable carbon source (electron donor) thereby releasing a chloride ion to become TCE (Azadpour-Keeley et. al., 2001). PCE and TCE can be completely dechlorinated to ethene through the sequential reduction reaction presented in Figure 28 in an anaerobic environment (Wilson, 1997). Also, PCB and TCE can be co- metabolically degraded in anaerobic environments (McCarty and Semprini, 1994). TCA can be reductively dechlorinated to DCA, which can be filrther dechlorinated to chloroethane (CA). CA is relatively recalcitrant to biological processes, but can be abiotically converted to ethanol (McCarty and Semprini, 1994). 70 Biotic Degradation Processes: Rate Sensitivity to Redox Conditions The redox conditions of the groundwater system control the relative rates of degradation. Reaction rates are much higher for reductive dechlorination processes when strongly reducing conditions exist, such as methanogenesis, than when weaker reducing conditions exist, such as denitrification. Also, it has been observed that anaerobic transformation rates are higher for the more chlorinated compounds (i.e. PCE, TCE, and TCA) than the less chlorinated ones (DCE, DCA, and VC), because they are already relatively reduced (McCarty and Semprini, 1994). Lastly, aerobic transformations of the less chlorinated species (DCE, DCA, and VC) are much faster than the anaerobic pathways (Chapelle, 1997). CURRENT METHODS TO ESTIMATE FIELD SCALE DEGRADATION RATES The transport model of plume G required degradation rates as input parameters; therefore; a literature review was completed to determine the best method to estimate the field scale degradation rates of plume G compounds. The review revealed three methods that are currently used. Wiedemeier et. al. (1996) provides a detailed description of two of the methods, which are tracer normalization and a method derived by Buscheck and Alcantar (1995). The third method involves adjusting degradation rates in a numerical model to match field data and was demonstrated recently by Clement et. al. (2000). A description of the methods is provided along with the advantages/disadvantages of each. Tracer Normalization Wiedemeier et. al. (1996) presented a method to estimate field scale degradation 71 rates between two points along a flow path, which was referred to as tracer normalization. Recalcitrant organic or inorganic compounds associated with the contaminant plume are used as tracers to quantify the non-destructive attenuation mechanisms. Two tracers that are commonly used are trimethylbenzene (TMB) isomers, which are only present if fuel hydrocarbons are a co-contaminant, and chloride. The first step is to normalize the contaminant concentration at a downgradient point using the following equation: CB corr : CB[T—A] . TB where C 3w, = corrected contaminant concentration at point B downgradient of A CB = measured contaminant concentration at point B TA = tracer concentration at a point A upgradient of B TB = tracer concentration at point B downgradient of A The corrected value is the anticipated concentration that would result if dispersion and dilution had not occurred between points A and B. The corrected value theoretically reflects only contaminant degradation. The first order decay rate between the two points can be calculated using the following equation: C _ -N B,corr where C3,“,rr = normalized contaminant concentration at downgradient point B CA = contaminant concentration at upgradient point A h = first-order biological decay rate [I/T] t = travel time from point A to point B for the given contaminant The advantages of tracer normalization are that it is relatively straightforward, the calculations are easy and take minimal time, and the results are readily available to 72 compare with other study sites. However, several drawbacks exist to the tracer normalization method. The primary contaminants and their daughter byproducts are usually the only compounds quantified during a sampling event. As a result, tracer data are often not available to perform the normalizations. Even if tracer data are available, the method assumes that the two points where the contaminant concentrations were measured lie along a flow path and that the travel time between the two points is known. Unless the flow regime has been studied extensively and subsequent sampling points sited in a manner to incorporate flow paths, the results would be questionable. Semi-Graphical Method of Buscheck and Alcantar (1995) Buscheck and Alcantar (1995) derived a semi—graphical method to estimate field scale degradation rates and Wiedemeier et. al. (1996) indicated that the method is an alternative to the tracer normalization method. First, a In-linear plot is constructed with contaminant concentration plotted relative to distance along a flow path. Once the plot is created, the first order decay rate is calculated from the following equation: 2 h: V“ [1140(1)] —1 4a,r v" where h = first-order biodegradation rate constant vC = retarded contaminant velocity in the x direction 01,, = longitudinal dispersion k/vx = slope of the line formed by making a ln-linear plot of contaminant concentration relative to distance along a flow path The semi-graphical method requires less data than the tracer normalization method, it is also simple and straightforward, and the results can be readily compared to published 73 rates in order to compare the site to other research areas. There are some disadvantages to the semi-graphical method. First, the equation was derived for a steady state plume. Determining that a plume is at steady state requires a large data set collected through time to ensure that steady state conditions exist, which is expensive and the data are often not available. In addition, the equation only applies to l-D systems and is therefore limited for complex 3-D flow systems. Numerical Modeling Field scale degradation rates can be estimated by calibrating a numerical model to field data. Clement et. al. (2000) provides an example of this methodology through research conducted at the Dover Air Force Base in Delaware. The authors created a 2-D flow and reactive transport model based on site-specific geologic, hydrogeologic, and geochemical data. Mesocosms were used to determine laboratory rates of degradation, which served as a starting point during their model calibration. The degradation rates were bounded during the calibration process by the literature values presented in Wiedemeier et. al. (1996). The objective function of the process was to match calculated observed contaminant masses to model predicted contaminant masses. The model successfully predicted contaminant distributions and reproduced contaminant masses adequately. An advantage of the method is that it considers processes controlling the whole plume, not just those occurring along a 1-D flow path, and therefore can be applied to 3-D field problems. As with the other methods, some drawbacks exist. Creating a site- specific model is labor intensive and requires much more data than the two previously described methods. Also, it is difficult to match observed contaminant masses when there 74 is almost always limited knowledge of the location and amount of all the contaminant inputs to the system. Method to Estimate Rates at Plume G A numerical modeling method was used to estimate field scale degradation rates of plume G compounds. Ideally, the other two methods could be used to calculate rates to constrain the model calibration and to better understand the relative rates of degradation. However, no tracer data were available for plume G, thus the tracer normalization method could not be used. Also, sampling point locations in plume G were not conducive to the semi-graphical method. As a result, the transport model was solely used to estimate field scale degradation rates of plume G compounds. CONCEPTUAL MODEL The conceptual model approach was used to develop the plume G transport model. The literature review of the past site investigations provided a framework for model stress periods. Geochemical data were evaluated in order to determine the predominant degradation reactions in the aquifer and to identify possible redox zones. A method to calibrate the model was then developed. The calibration procedure is a new approach that was developed for plume G, but may prove useful at other sites where source compounds have transformed. Model Stress Periods Multiple stress periods were needed to adequately simulate plume G. A timeline 75 of events at ARCO is presented below to summarize activities that potentially affected numerical simulations (Everett, 1990). 1953 — Rubber and plastic auto parts manufacturing facility on Eliza Street in Schoolcraft, Michigan opens and presumably, improper storage and disposal of source chemicals begins at Areas 1, H, and ID. 1965 — Wastewater drainage was diverted from the Area H pond to the South Seepage Pond. 1967 — Arco Industries Corporation assumes ownership and operation of the manufacturing facility on Eliza Street in Schoolcraft. 1985 — The Michigan Department of Natural Resources identifies ARCO as a source of contamination of the groundwater downgradient of the site property. June 1987 to September 1988 — The Area I soil vapor extraction system tests remove 110 kg of chlorinated solvents from the vadose zone. 1988 — Production of plastic/rubber parts and use of solvents is discontinued at ARCO. June 1988 — Approximately 115 m3 of contaminated sludge were excavated from the northeastern section of the South Seepage pond. May 1989 — Approximately 64 m3 of contaminated sludge were excavated from the southeastern section of the South Seepage pond. July 13, 1992 — PW-3 began extraction of groundwater from the aquifer to an off- site air stripping tower. The well discharges at 1090 m3/day and is still in operation. This timeline reveals that site usage has varied throughout the facility’s existence, therefore recharge rates and source concentrations were different at each area, which required multiple stress periods for the transport model. The four source areas were determined to have elevated levels of recharge based on knowledge of past on-site activities. Areas 1 and IH were used as general clean-up areas where objects were washed with a variety of solvents and water, thereby increasing recharge. The duration of elevated recharge at these sites were assumed to exist from the 76 plant’s startup in 1953, until operations effectively ceased in 1988. The Area H pond and the South Seepage pond held pools of standing wastewater and were subsequently areas of elevated recharge that were higher than the recharge at Areas I and 1H. Area H was only used from 1953-1965, and the elevated recharge was assumed to occur during that period. The South Seepage pond was assumed to be an area of elevated recharge from its opening in 1965 until the first excavation in June of 1988, when the pond sediments had fully dried. The recharge at the source areas acted to deliver contaminants to the groundwater as water infiltrated and replenished the aquifer. Estimating the source term in a contaminant transport model is a difficult task; therefore, several assumptions were made to deal with the source problem. First, the degree of contamination was found to be variable from area to area, but the concentration at a given site was assumed constant. Information provided in the description of the site background indicated that the degree of contamination varied from highest to lowest in the following order: Areal, Area HI, Area H, and the South Seepage pond. Second, Areas 1, H, and HI were assumed to be source areas from the time the facility opened in 1953 until the end of the model simulation. Justification for this assumption lies in the fact that significant contamination was detected at all of the sites during investigations in the late 1980’s and early 1990’s and that no significant source removal operations were enacted at any of the three sites in the past. Even though the SVE system removed 110 kg of chlorinated solvents from the vadose zone in Areal, it was conservatively estimated that at least 10,000 kg of PCB and 13,000 kg of TCE were present within the top 2 m of sediments at Areal. The removal of 110 kg of chlorinated organics was essentially minimal and was not expected to decrease the source term. The South Seepage Pond was 77 assumed to be a source from its opening in 1965 until the first excavation in June of 1988. The unexcavated portion of the pond was considered a source from 1965 until May of 1989 when the final remnants of contaminated pond sludge were removed. The final excavation was assumed to have completely removed the South Seepage pond as a source since subsequent sampling of the soils below and adjacent to the pond indicated that little or no residual contamination remained (Everett, 1990). Analysis of the aforementioned site history revealed that since the ARCO plant opened in 1953, there were four periods where recharge rates and/or source locations varied and one period when the heads changed due to drawdown from a pumping well. A summary of the five periods is presented in Table 6. Note that the table indicates whether recharge was elevated (yes/no) and if the area was a source (yes/no) during that specific period. Also, only the southern half of the South Seepage pond was a source in the third stress period since the northern half of the pond was excavated in June of 1988. The specific quantitative values for source recharge rates and concentrations were assigned later, when the model was created. The stress period that starts on 5/5/1992 was the result of the activation of PW-3, which influenced the heads near the downgradient end of the plume. The resulting head distribution from PW-3 can be incorporated into a second plume scale model in which the heads were derived from the regional model that included PW-3 and the initial concentrations of plume G species were derived from the first transport model that ended on July 13, 1992. It should be noted that not all five of the stress periods were incorporated in the RT3D model due to the limited observed data that were available past 1989 (this is explained later in the thesis in the Conceptual Calibration section). 78 Table 6. Summary of conceptual stress periods for plume G transport models. Duration Area I Area II Area 111 SSP Period (start/stop) recharg source recharge source recharg source recharge source 1 ““1953 yes yes yes yes yes yes no no 1/1/1965 2 In“ 965 yes yes no yes yes yes yes yes 6/27/1988 3 £25132: no yes no yes no yes no 1/2* 4 5/8/1989 no yes no yes no yes no no 5/5/1992 5/5/1992 5** no yes no yes no yes no no present recharge - yes = elevated recharge, no = plume scale model recharge (12 cm/year) * Only the southern half of the pond was a source during this stress period ** PW-3 was in operation this time period Conceptual Reactions of Interest The literature review of the degradation processes revealed that the reactions are complex and are controlled by the redox state of the aquifer; therefore, geochemical data were examined to determine the probable degradation pathways of plume G compounds. Eight data sets were available for interpretation of processes. Seven data sets were collected by ARCO consultants from 1988-1996; however, five of the datasets only contained results from 5-6 wells, and thus were not very helpfill in determining potential process on the plume scale. Also, the ARCO data sets only contained results for the chlorinated compounds present in plume G; no redox analyses were performed. The eighth data set consisted of samples collected and analyzed by the Civil and Environmental Engineering Laboratory at MSU from nine MSU monitoring wells in plume G. Redox analyses were performed during the MSU sampling event and were used to identify possible redox conditions in the aquifer. 79 Analyses of samples from the MSU sample grid were conducted by the Civil and Environmental Engineering Laboratories at MSU in February of 2001. The results showed that elevated levels of nitrate existed until a depth of about 13 meters below ground surface (mbgs) where the levels subsequently decreased with increasing depth until the bottom of the aquifer at a depth of about 26-27 mbgs (Figure 29). Chappelle (1993) indicated that if there is a source of nitrate in a system, it will accumulate in an aerobic environment and will be reduced and decrease in concentration in an anaerobic system. The results indicate that the aquifer at the site of the MSU sample grid is aerobic to a depth of approximately 13 mbgs and anaerobic to the base of the aquifer at approximately 26-27 mbgs. The anaerobic zone can be further split into a zone of denitrification from 13 mbgs to 19 mbgs where nitrate decreases with depth until it becomes almost depleted, which indicates that the aquifer may be in a more reducing state from 19 mbgs to the clay layer at about 27 mbgs. No other redox data specific to plume G were available and the redox conditions throughout the plume were assumed to be the same as those delineated at the MSU sample grid. Subsequently, both the aerobic and anaerobic pathways of degradation depicted in Figure 28 were included in the model of plume G reactions. Examination of Figure 28 shows that there are two sources of 1,1-DCE in an aquifer if TCA and TCE are present. Most TCE degrades to the cis— isomer of 1,2-DCE, with only minor amounts transformed to the trans- isomer of 1,2-DCE, and even less to 1,1-DCE (Chappelle, 1993). McCarty (1997) indicated that if TCA were present in an aquifer, the predominant transformation pathway would be the biotic route and that the abiotic transformation to 1,1-DCE would be negligible. If abiotic transformation of TCA 8O Nitrate (ppm) 0 10 20 30 4O 50 6O 70 80 0 I T I I I I ITI WTI T r I I I T T I I T I I I I f7 T—r T T I_T I I T I I I I 5 l ............................................ i, ......................................... 1 I; _l Depth Below Ground Surface (m) _ . - '6 ” 1 15 ._.. ............. . ......................... ........................................... _. _ {O - l . - r : i 20 ,._............... , ............................................. .2 >— . z E —l l o - o? - ‘ - - . 7 25 I Lgl l I 1 Ill 1 1 Lil 1 L411 1 I l IJ_LI I l I I 14 J 1_L11 .1 N ‘1 O 5 A A ‘ ‘ A A ‘ D D... D D ‘ NUS Monitoring Well I MSU Monitoring Well Figure 29. Nitrate concentrations at monitoring well MSU-5 from February, 2001. Note that nitrate starts to decrease at about 13 mbgs until about 19 mbgs, where it remains constant. Results suggest that the aquifer is aerobic from the water table to 13 mbgs, anaerobic denitrifying from 13 mbgs to 19 mbgs, and somewhat more anaerobic from 19 mbgs to the clay at about 26-27 mbgs. 81 was negligible, then the TCA pathway to VC could essentially be ignored. However, observed concentrations of 1,1-DCE throughout the entire plume ranged from 0-360 ppb. Although some 1,1-DCE forms as the result of the degradation of TCE, McCarty (1997) indicated that if 1,1-DCE were present in an aquifer, it was most likely the result of the abiotic transformation of TCA. As a result, the TCA degradation reaction was a potentially significant source to vinyl chloride production and was included in the model of plume G reactions. All of the conceptual reactions depicted in Figure 28 were assumed to occur at plume G, except that 1,1-DCE was assumed to only form from the abiotic transformation of TCA. Conceptual Method of “Calibration ” Calibration of a model typically involves adjusting model parameters until a minima in an objective function is achieved, such as sum of residuals between measured and calculated concentrations. Transport models are often calibrated by predicting the center of mass of each species in the plume, or by predicting observed concentrations at monitoring points within the plume (Bedient et. al, 1999). However, contaminant plumes are often poorly characterized by observed data; plume G was no exception. Limited data were available for the plume G study; subsequently, traditional methods of calibration were not employed. Observed data were analyzed at a downgradient well transect. The model was calibrated by comparing the simulated results to the observed results at the monitoring well transect. Several key problems existed with the plume G data set that limited comparisons of simulated and observed concentrations. First, samples were not analyzed for chloride. 82 If chloride concentrations were known, then the mass of each source could be better estimated through methods presented by Wiedemeier et. al. (1996). Second, there were only two data sets (May, 1988 and June, 1989) where sufficient data existed throughout the plume area, but a consistent set of wells were not sampled during the two different sample events making temporal comparisons of the simulation results difficult. Subsequently, the model was considered a preliminary model and was compared to the June 1988 data set, which meant that only stress periods 1 and 2 of Table 6 were incorporated into the model. A transect of wells perpendicular to plume G was located approximately 650 meters downgradient of ARCO where observation data for June of 1988 were available (Figure 30). The transect was about 450 meters wide and consisted of 18 wells. The wells were not true multilevel wells in a single borehole, but a series of 3 wells within a few meters of each other in the horizontal plane where each well was screened at a different elevation. TCE concentrations at the transect are plotted in Figure 31. Note that there is a significant difference in concentrations, even at points that are somewhat close to each other, such as MW-44A and MW-44B where concentration changes from 580 ppb to 3700 ppb with only 3 meters difference in the vertical distance between the points. Possible explanations for the differences are the variable redox conditions of the aquifer and/or preferential flow paths in the aquifer. The geologic heterogeneity of the aquifer that was represented in the plume scale flow model did not include small gravel lenses or other small preferential flow paths. As a result, the plume scale flow model was not expected to predict the point observed values at the transect, but it was expected to predict the relative mass of each species in three conceptual contamination zones defined 83 by the redox conditions at the transect. The model was used to predict the vertical distribution of contamination in three conceptual contamination zones at the monitoring well transect depicted in Figure 31. First, the transect was divided into three zones based on the previously delineated redox conditions. The shallow zone corresponded to layers 1-4 (0 to 13 mbgs) of the plume scale flow model and was aerobic. The middle contamination zone correlated to layers 5- 7 (13 to 19 mbgs) of the plume scale flow model and was anaerobic (denitrifying). The deep contamination zone correlated to layers 8-10 (19 to approximately 27 mbgs) of the plume scale model grid and was somewhat more anaerobic than the middle zone based on Figure 29. The observed mass of each contaminant (PCE, TCE, 1,2-DCE, 1,1-DCE, TCA, DCA, and VC) in the aqueous phase was estimated using Theissen polygons in the vertical plane and assuming an aquifer thickness equal to the diameter of the monitoring wells (10 cm) and a porosity of 0.375 (Hoard, 2002). The calculated observed masses for each species are summarized in Table 7 and were the basis for comparisons with the simulated results. The model results would need to be analyzed to determine the simulated mass of each compound in the shallow, middle, and deep contamination zones at the monitoring well transect for comparison with the estimated observed masses. The simulated mass in each zone was not calculated with Theissen polygons because simulated data were available for each grid cell at the transect, therefore data did not need to be interpolated with the polygons. The aqueous mass of each species was calculated for each cell using the cell area in the vertical plane multiplied by the width of the wells (10 cm), the porosity, and the aqueous concentration that was simulated for the given cell. The 84 calculated masses for the cells in the three zones were summed to yield simulated masses for the three contamination zones at the same location where observed masses were estimated. mbgs, 1.07x105 L) zones for June of 1988. Table 7. Estimated total aqueous mass of observed compounds at well transect in shallow (0-13 mbgs, 1.44x105 L), middle (13-19 mbgs, 1.36x105 L), and deep (19-27 Zone PCE (g) TCE(g) 1,2-DCE (g) TCA (g) DCA (g) 1,1-chg) veg; Shallow 2.37 68.15 13.93 14.32 0.18 0.91 0.00 Middle 4.53 93.22 15.70 16.75 0.33 0.94 0.00 Deep 9.02 95.54 37.71 16.41 4.98 2.97 8.32 Totals 15.92 256.91 67.34 47.48 5.49 4.82 8.32 The calculated simulated and observed masses for the downgradient transect were used to check the source zone concentrations and then to adjust the model degradation rates to calibrate the model. Initially, simulated masses were compared with the estimated observed masses in Table 7 to ensure reasonable source concentrations. However, since there was so much uncertainty in the source term, the objective function of the calibration was to match the ratio of the mass of each species to the mass of its daughter byproduct in each zone (i.e. PCE/TCE for the shallow zone = 2.37/68.15 = 0.0348). The ratios are independent of the absolute mass of each compound. Even if the simulated mass is not equal to the observed mass, the model can represent plume G processes if the mother/daughter ratios that are calculated from the simulated masses reasonably match the calculated ratios from the observed data. 85 {L N " A _ A A L /' A ‘ A A A A ‘ ‘ ‘ A A NUS Monitoring Well 0 500 I MSU Monitoring Well meters Figure 30. Location of downgradient monitoring well transect used to identify vertical zones of contamination. The numbers correlate to the NUS number assigned to the wells during the remedial investigation studies in the late 1980’s (Mayotte, 1991). 86 TCE (ppb) Jh Middle — Anaerobic Jll\ Depth Below Ground Surface (m) [It-up .\ll;1l:lllhlt‘ (more reducing) Jllli 300 Width (m) Figure 31. Plot of TCE concentrations at a well transect perpendicular to groundwater flow approximately 650 meters downgradient of the ARCO facility. The shaded regions are the shallow, middle, and deep generalized zones of contamination. The view is looking ugradient towards ARCO. Image is presented in color. 87 IMPLEMENTATION OF THE CONCEPTUAL MODEL The transport model was implemented as an RT3D model through GMS using the flow model created in Chapter H1. The first step was to develop a reactions package to mathematically represent the conceptual degradation reactions presented in Figure 28. The model parameters required by the equations were then assigned; among which were the porosity, dispersivity, retardation factors, contaminant yield factors, and initial degradation rates. The source boundaries were then assigned and the model was calibrated according to the method outlined in the Conceptual Calibration section. Creation of an RT 3D Reactions Package The 3-D advection-dispersion equation with first order decay was solved using RT3D (Clement, 1997). RT3D is a modular computer code for simulating reactive transport in three-dimensional groundwater systems. The code uses a reaction operator- split numerical strategy to separate the components of the transport equations so that the coupled partial differential equations that describe reactive transport can be assembled as a set of ordinary differential equations and solved separately from the advection- dispersion portion of the equation. The equations are coded according to an RT3D specified format into a reactions package that is compiled as a dynamic link library file and used by RT3D to solve for the concentrations of the user-defined species (Clement, 1997) The coupled set of ordinary differential equations equations representing the conceptual degradation model presented in Figure 28 are as follows (note that these 88 equations represent only the degradation reactions; advection and dispersion are also simulated in the model, but not with the equations below): d[PCE] _ - KPCE[PCE] dt RPCE leCE] : YTCl-L‘PCE K PCE [PCE] ' KTCE1[TCE] ' KTCEz [TCE] dt R TCE d[1,2 - DCE] : er-DClarcrz KTCE1[TCE] ‘ Kl.2-DCE1[1’2 ' DCE] ' Kl,2-DCE2 [1’2 ' DCE] dt Rl,2-DCE leCA] : ' KTCA-A [TCA](A) ‘ KTCA-Bl [TCA](B) ’ KTCA-BZ [TCA](B) dt RTCA d[191' DCA] = (B)Yl.l-DCA/TCAKTCA-Bl[TCA] - I<-< r< where [PCE], [TCE], [1,2-DCE], [TCA], [1,1-DCA], [1,1-DCE], [VC], [CA], [Ethene], [Ethanol], and [C1] are contaminant concentrations [ppb]; Kpcg, Kresr, Kl,2-DCEl, KTCA-31, K1,1-DCA1, Kl,l-DCE1, Kym, KEthener, KEthanol are the first order anaerobic biodegradation rates [day"]; Krcaz, Kl,2-DCE2, KTCA-BZ,K1,1-DCA2, K1,1-DCE2,KVC2,I(Ethene2 are the fifSt order aerobic biodegradation rates [day-1]; KTCM, and KCA, are the first order abiotic degradation rates [day"]; and RPCE, RTCE, RTCA, Rl,2-DCE, Rl,1-DCA, Rl,l-DCE, va. RCA. Rgthene, REthanol are contaminant retardation factors. The yield factors (Y) are dependent on the stoichiometry of the reaction and the molecular weights of the compounds. An example calculation for the anaerobic degradation of PCE is that one mole of PCE degrades to become one mole of TCE, or YTCEjPCE = molecular weight of TCE / molecular weight of PCE (131.4 g/mol/ 165.8 g/mol = 0.79). The abiotic (A) and biotic (B) factors account for the two major paths that TCA is degraded and were adjusted during model calibration since no values were reported in the literature (note A+B=1). The 0.79 and 0.21 factors account for the observation that in the abiotic pathway of TCA degradation, 79% of TCA degrades to ethanol and 21% degrades to 1,1-DCE. Note again that it was assumed that the sole source of 1,1-DCE in the system was the abiotic degradation of TCA based on McCarty (1997). Although the equations include 90 chlorethane (CA), ethene, ethanol, and chloride, there were no observed data for these compounds to compare to the RT3D simulated values. These components were included in the reactions package for future modeling exercises of plume G. Assignment of Model Parameters The transport model required many input parameters, which were applied to the model in GMS. The advection/dispersion parameters were assimilated from field studies in the area and from the literature. The source concentrations were estimated from results of the initial site investigations of the area (Everett, 1990). The source zone infiltration rates were calculated from methods presented in the literature. Initial degradation rates were applied to the model based on results presented in Suarez and Rifai (1999). The advection and dispersion properties of the transport model were assigned in GMS. The porosity value that was used was 0.375, which was an average value determined from sieve analyses at plume A (Hoard, 2002). The retardation factors were estimated by a method presented in Bedient et. al (1999) (Table 8). It is typically useful to have site-specific retardation factors determined by batch reactions with material obtained from the site, but since the model of plume G was one of the first studies completed, retardation factors were not available. The longitudinal dispersivity that was applied to the model was 3 m based on an overall travel path of 1340 m using a relationship presented in Xu and Eckstein (1995). The ratio of horizontal to longitudinal dispersivity that was used was 0.1 (Aziz et. al., 2000) and the value of vertical to longitudinal dispersivity was 0.05 (ASTM, 1995). The porosity, retardation factors, and 91 dispersivity values remained constant during model calibration (Table 8). Table 8. Summary of transport model parameters which remained constant throughout model calibration. RPCE 2.50 YTCWE 0.792 YCWCE 0.270 RTCE 1-60 Y1 ,Z-DCE/TCE 0-738 Yer/1.2-003 0-366 Rm),-E 1.22 Y,,,.DCA,TCA 0.742 Y0,TCA 0.266 RTCA 1.66 10,..meTCA 0.727 Yew.DCE 0.366 R1 ,l-DCA 1-18 YEthanol/TCA 0450 Your ,l-DCA 0-358 Rum-E 1.31 vawcE 0.645 YCVCA 0.550 RVC 1.09 YVW.DCE 0.645 00* 3 m RCA ### YCM,,-DCA 0.652 002011" 0.1 REthene #44 1{E,,,,,,,.,VC 0.449 over“ 0.05 REthanol ### YEthanol/CA 0-931 11"" 0-3 75 RC. 1.00 YCWCE 0.214 Rspccies - Retardation factors calculated fiom Bedient et. a1. (1999) ## - Observed data were not available; retardation factors not needed Yspecimpecies - Yield factors calculated from molecular weights * - Longitudinal dispersivity calculated from Xu and Eckstein (1995) ** - Transversezlongitudinal dispersivity from Aziz et. al. (1999) *** - Vertical:longitudinal dispersivity from ASTM (1995) **** - porosity from Hoard (2002) The model was divided into stress periods 1 and 2 that were outlined in Table 6 in order to assign the various recharge and source values to the model. A recharge rate of 0.065 m/day was estimated for the ponds (Area H and the South Seepage Pond) using a method presented by Youngs et. al. (1996). The source recharge rate for Areas I and H] was assumed to be equal to half of the value for the ponds (0.0325 m/day). An average soil concentration of each of the source species was determined from results presented in Everett (1990). Distribution coefficients determined from Bedient et. al. (1999) were used to estimate the aqueous concentration, assuming equilibrium partitioning, at the 92 contaminated source soils. The aqueous concentrations were assigned as recharge boundaries in the RT3D model (Table 9). The source recharge rates and source concentrations remained constant during the model calibration process. Table 9. Estimated source concentrations for the model source areas based on site investigation results assimilated in Everett (1990). Source Contaminant PCE TCE TCA 80"“ Am Kd (L/kg)* 0.48 0.13 0.15 Area I Soil Conc.(ug/kg) 70000 70000 14000 Aqueous Conc. (pg/L) 145833 538462 93333 Area H Soil Conc.(ug/kg) 150 210 0 Aqueous Conc. (jig/L) 313 1615 0 Area HI Soil Conc.(ug/kg) 20000 20000 15000 Aqueous Conc. (pg/L) 41667 153846 100000 South Seepage Soil Conc.(1lg/kg) 100 100 20 Pond Aqueous Conc. (lg/L) 208 769 133 * Estimated by method presented in Bedient et. al. (1999) The first order degradation rates were the last parameters assigned to the transport model. The model includes aerobic and anaerobic biodegradation rates, as well as abiotic decay rates. However, it was determined previously that the top four layers of the model existed under aerobic conditions, while the bottom six layers were anaerobic. Therefore aerobic rates (TCE2, TCA-B2, 1,2-DCE2, 1,1-DCE2, DCA2, VC2) were zero in anaerobic zones, and the anaerobic rates (TCEl, TCA-Bl, 1,2-DCE1, 1,1-DCE1, DCAl, VCl) were zero in the aerobic zones. PCE does not degrade under aerobic conditions and therefore the decay rate was zero for PCE in layers 1-4 (the shallow aerobic zone). The abiotic TCA rate was determined by several authors to be solely a function of temperature; therefore, the TCA abiotic rate was taken from McCarty (1997) based on a temperature of 15°C and remained constant in all 10 layers. The initial values that were 93 assigned for all other rates were the mean value determined by a literature search that was completed by Suarez and Rifai (1999). The authors compiled a list of first order degradation rates for chlorinated ethenes/ethanes and results are presented in Table 10. Table 10. Summary of first order decay rates for chlorinated compounds as comfled by Suarez and Rifai (1999). Species Low (day") Higflday") Mean (day-1) PCE 0 0.41 0.051 TCEl 0 3.13 0.086 TCE2 0 1.65 0.346 1,2-DCE1 0 0.2 0.004 1,2-DCE2 0 1.96 0.476 TCA-A* 0.000375 0.000397 0.000383 TCA-Bl 0 2.33 0.355 TCA-B2 0 1.18 0.079 DCAl 0 0.044 0.036 DCA2 0 0.131 0.048 1,1-DCE1 0 0.27 0.019 1,1-DCE2 0 1.15 0.458 VCl 0 0.52 0.153 VC2 0.043 0.12 0.55 * values summarized by McCarty (1997) for a temperature of 15°C 1 = anaerobic rate , 2 = aerobic rate MODEL CALIBRATION The biodegradation rates were adjusted during model calibration, but were constrained between literature values presented in Suarez and Rifai (1999) and adjusted based on knowledge of relative rates of degradation according to the redox conditions. Chappelle (1997) indicated that the aerobic degradation rates for the less chlorinated species (DCE, DCA, VC) were higher than the anaerobic degradation rates, and this was a constraint on rate adjustment. Also, the aerobic degradation rates should increase from 94 TCE to DCE to VC and from TCA to DCA (Chappelle, 1997), and this was also a constraint on the parameter adjustment. Lastly, anaerobic rates increase as the system becomes more reducing, therefore the anaerobic rates in the deep zone (layers 8-10) were constrained to be higher than the anaerobic rates in the middle zone (layers 5-7). These constraints helped to focus the calibration process. Results The simulated mass for each species in the three conceptual contamination zones is listed in Table 11, while the mother/daughter ratios are in Table 12. Note that there was no mass of vinyl chloride in the shallow and middle zone, but a calculated ratio was needed to evaluate the model. As a result, the detection limit of 1 ppb was used to calculate a mass for the shallow and middle zones so that ratios could be calculated without dividing by zero. The model reasonably predicts the total mass of each species at the monitoring well transect, except PCE concentrations are somewhat low. The general trend in the vertical distribution of the masses is consistent with the observed trend as well. However, there is too much 1,2-DCE, DCA, 1,1-DCE, and VC in the middle zone. The mother/daughter ratios of the middle zone help to depict this problem (Table 12). The residuals of the ratios in the middle zone are all too low, indicating that the mass in the middle zone is too high. The calibrated rates used in the model simulations are given in Table 13 along with the model determined abiotic (A) and biotic (B) TCA factors. The rates are within the range of observed values tabulated by Suarez and Riafi (1999). The model rates are somewhat low compared to the observed ranges listed in Table 13. Explanation for lower 95 rates is that the tabulated values were taken from a variety of redox conditions and some were taken from laboratory studies, both of which may be different from the Schoolcraft site. However, the model rates are similar (10'3 to 10'5 day") to the field scale rates determined by Clement et. al. (2000) for the Dover site. The abiotic (A) and biotic (B) factors account for the relative amount of TCA that is transformed biotically or abiotically; it is a mass balance term and therefore A+B=1. The model determined A and B factors were 0.4 and 0.6 respectively. If an abiotic factor less than 0.4 (which also corresponded to a biotic factor that was greater than 0.6) was used, the 1,1-DCE mass was too low and the DCA mass was too high. Table 11. Observed and simulated masses for the three conceptual contamination zones outlined in the Conceptual Calibration section. OBSERVED MASS PCE TCE 1,2-DCE TCA DCA 1,1-DCE VC shallow 2.37 68.15 13.93 14.32 0.18 0.91 0.00 middle 4.53 93.22 15.70 16.75 0.33 0.94 0.00 deep 9.02 95.54 37.71 16.41 4.98 2.97 8.32 total 15.92 256.91 67.34 47.48 5.49 4.82 8.32 SIMULATED MASS PCE TCE 1,2-DCE TCA DCA 1,1-DCE VC shallow 0.49 66.46 8.26 l 1.56 0.16 0.95 0.06 middle 1.43 93.95 26.15 17.26 2.30 2.16 6.61 deep 1.95 98.38 37.80 17.32 3.24 2.50 16.97 total 3.87 258.79 72.21 46.14 5.70 5.61 23.63 RESID UALS (SIM ULA TED - OBSER VED) PCE T CE 1,2-DCE T CA DCA 1,1-DCE V C shallow -1. 88 -1. 69 -5. 67 -2. 76 -0. 02 0.03 0. 06 middle -3.11 0. 73 10. 45 0.50 1.97 1.23 6. 61 deep -7. 06 2.84 0.09 0.92 -1. 75 -0.4 7 8. 65 total -12. 05 1.88 4.87 -1.34 0.20 0. 79 15.31 96 Table 12. Observed and simulated contaminant mother/daugher ratios for the three conceptual contamination zones outlined in the Conceptual Calibration section. OBSERVED MOTHER/DAUGHTER RATIOS PCE/TCE TCE/Dela" DCE’WC TCA/DCA TCA/DCE* DCE*/VC shallow 0.035 4.893 103.165 80.070 15.666 6.771 middle 0.049 5.938 112.141 51.193 17.916 6.680 deep 0.094 2.534 4.532 3.291 5.526 0.357 SIMULATED MOTHER/DAUGHTER RATIOS PCE/TCE TCE/DCE“ 13013th TCA/DCA TCA/DCE“ DCE*/VC shallow 0.007 8.049 140.987 72.539 12.214 16.164 middle 0.015 3.592 3.959 7.502 7.975 0.328 deep 0.020 2.603 2.228 5.353 6.925 0.147 RESID UALS (SIMULA TED - OBSER VED) PCE/TCE TCE/DCE “ DCE#/VC TCA/DCA TCA/DCE“ DCE*/VC shallow -0027 3.156 37.822 -7531 -3452 9.393 middle -0. 033 -2345 -108.182 -43.691 -9941 -6.352 deep -0075 0.069 -2304 2.062 1.399 -0209 # - TCE/DCE and DCE/V C were calculated using the 1,2-DCE isomer * - TCA/DCE and DCE/V C were calculated using the 1,1-DCE isomer Table 13. Summary of calibrated parameters used in the RT3D model. First Oder Description Shallow Aerobic Middle Anerobic Deep Anaerobic Rate Zone (day-l) Zone (day-1) Zone (day-1) PCE anerobic l .0E-05 1 .0E-04 TCEl anaerobic 1.35E-04 2.50E-04 TCE2 aerobic 1 .1 5E-04 1,2-DCE1 anaerobic 1.00E-04 4.00E-04 1,2-DCE2 aerobic 1 .00E-03 TCA-A abiotic 3.83E-04 3.83E—04 3.83 E-04 TCA-B 1 anaerobic 2.50E-04 6.00E-04 TCA-B2 aerobic 1 .00E-04 DCAl anaerobic 9.49E-04 9.50E-04 DCA2 aerobic 6.10E-03 11DCE1 anaerobic 1.00E-04 4.00E-04 1 1DCE2 aerobic 9.50E-04 VCl anaerobic 9.99E-05 1 .00E-04 VC2 aerobic 4.30E-02 A=O.4 B= 0.6 97 Model Sensitivity to Degradation Rates The RT3D model is a numerical approximation to a complex problem and the solution may not be unique. The range of observed degradation rates for the species present in plume G is large (Table 10). Simply calibrating the model by matching the mother/daughter ratios could lead to an erroneous solution if other factors such as plume extent were not examined. Preliminary sensitivity simulations helped to identify a range of probable degradation rates in which the observed plume extent was appropriately predicted. Sensitivity simulations were then run to determine if the modeled rates were the optimal rates for the model. The final rates used in the model were on the order of 10'2 to 10'5 day'1 with most rates on the order of 10‘4 day'l. The range was determined from multiple preliminary simulations, which served to Show model sensitivities to the degradation rate. The preliminary run used the mean degradation rates listed in Table 10, but these rates were much too high (the source species were degraded too fast and thus the plume had not moved far enough downgradient to observed positions). The subsequent runs were completed by decreasing all of the biodegradation rates by a factor of 10, 100, 1000, etc. The results showed that the degradation rates of PCB, TCE, and TCA were the most important parameters because they controlled the production of the daughter byproducts. Using rates for the source species that were less than the final rates (10'6 day'l instead of 10" day‘l) resulted in too much mass in the system, which subsequently moved too far downgradient of observed positions. The opposite was true if the rates for the sources species were higher than the final rates (10'2 day1 instead of 10‘4 day'l). The preliminary simulations provided useful information by narrowing the range of possible parameters. 98 Multiple simulations were run to evaluate the model sensitivity to changes in degradation rates. The final model rates listed in Table 13 were assumed to be the base case rates. The process involved changing the degradation rate of one species in one of the conceptual contamination zones (shallow, middle, and deep), while holding all other rates at the base case. As stated previously, the plume extent was sensitive to the PCE, TCE, and TCA rates, therefore, these rates were changed most from the base case values. The objective function was the root mean squared error (RMSE) of the mother/daughter ratios. Note that there were essentially two different sources in the system (PCE/TCE and TCA), which led to somewhat different degradation byproducts. Therefore, the objective function was calculated differently for the PCE/T CE pathway versus the TCA pathway. The RMSE for the PCE/TCE path was calculated based on the PCE/TCE, TCE/1,2-DCE, and the 1,2-DCE/V C ratios, while the RMSE for the TCA path was calculated based on the TCA/DCA, TCA/1,1-DCE, and the 1,1-DCEN C ratios. The results of the sensitivity simulations are presented in Figures 32-39. Figures 32-35 depict model changes in parameters that affected the PCE/TCE pathway, while Figures 36-39 depict model changes in parameters that affected the TCA pathway. The plots show that the modeled rates are at a minimum in the chosen objective function. Some plots (Figures 35 and 39) Show dashed lines that represent boundaries beyond which rates were not adjusted. Figures 35A and 39A show a boundary at 0.043 day", which is the literature minimum given in Table 10. Figures 35B and 39B are bounded by the constraint that the anaerobic rates in the middle zone cannot be higher than the deep zone (the deep zone is more reducing which favors stronger transformation rates). The plots also show that in general, the systems are most sensitive to decreases in the rates. 99 40 39 38 RMSE 37 36 35 40 39 38 RMSE 37 36 35 PCE Degradation Rate (day‘) T ' T T t Y * ' l * * _ L l I r. ......................................................................... .. .......................... .................. j * o O o a : Q . 1 Z Z : , : i— i l i L i l 1 l l r r i l L a r l l l .4 0 0.00002 0.00004 0.00006 0.00008 0.0001 0.00012 PCE Degradation Rate (day‘) * f T * r r r r f r r r _. l; ............... ' ............... g ................................. ..................................... B ,L >- O . . -< C 5 = 9 Z l : . . l. ...................................................................................................................... _1 C 1 e G - ._ ..................................................................................................................... —i P . i . l l . l i . . 1 l l l i . . i l l l A 0 0.0002 0.0004 0.0006 0.0008 0.001 0.0012 0.0014 Figure 32. Sensitivity plots of model error (RMSE) of the mother/daughter ratios (PCE/TCE path) in response to varying degradation rates (model rate is circled). A) The anaerobic PCE rate in the middle zone. B) The anaerobic PCE rate in the deep zone (note, PCE is not currently known to degrade under aerobic conditions, therefore there is no aerobic PCE rate in the shallow zone). 100 37.5 35 50 47.5 37.5 35 >- T T I T T Y T T T T T- -< I : é a a. ..... A .3 I o 3 E o 3 I o I i: ....................................................................................... : :0 _ . . . . 2 : . j I 2 I j ...... 9 _ E 9 g r 2 a s 4 : . = = s : l l . 1 l . . 1' l l A I l . . i l l A i . . l 7 0 0.0002 0.0004 0.0006 0.0008 0.001 0 0012 TCE-2 Degradation Rate (day‘) AT 1 r r r VVVVV r n -i :. ................................................................................ 3 I; ....... 9. ......... .................. .3 l- ; § 3 L. ................ 3 .......... .0 .......... _ .............................................................. g ................ 9.; l— : . j .4 Z S o 2 E3 ........................................................................ L '— 1 I a i L i . l i r l lllll 1 ..... 1 1 ML 1 i l . i r i i d 0 0.00006 0.00012 0.00018 0.00024 0.0003 0.00036 TCE-l Degradation Rate (day'l) __ f 4 a r r * ' r r * r * * ‘ 4 i- i -l 3? ............................................................................................................. C ..1 i 1 I 2 : o . : : 3 E 0 . 3 ~ 1 ° 0 : ‘ LQ. ............................. § ................. j ~ . i . . i . . j . . i . i . i . . . 0 0.0002 0.0004 0.0006 0.0008 0.001 0.0012 TCE-l Degradation Rate (day‘) 101 Figure 33. Sensitivity plots of model error (RMSE) of the mother/daughter ratios (PCE/TCE path) in response to varying degradation rates (model rate is circled). A) The aerobic TCE rate in the shallow zone. B) The anaerobic TCE rate in the middle zone. C) The anaerobic TCE rate in the deep zone. 95 85 75 65 RMSE 55 45 35 42 41 40 39 RMSE 38 37 36 95 85 75 65 RMSE 55 45 35 ’- 1 * fl * f f * fl * * I 7 fl _. 2 f A : E 3 5 3......W ........................................................................................................ _: C i »— . -1 :9 ............. j .............. 9 .................................................................... ; .................. _: : + 3 I : Q 1 1 i 1 944 1 1 1 i 1 1 . 1 1 1 . 1 1 1 Z 0 0.004 0.008 0.012 0.016 0.02 0.024 1,2-DCE-2 Degradation Rate (day") L # 1 f IV 1 r r l * * _ 1 f 3 o 1 r .......................... I. ................................ g 3 .......................... I ............................. , ................................................ B -_:. E I ‘ ° 3 E 1 3 E ........................................................................................................................ _: . . . 1 m1 . 1 . 1 . 1 . . . 1 1 . . i 1 . . i 0 0.00007 0.00014 0.00021 0.00028 0.00035 0.00042 1,2-DCE-1 Degradation Rate (day“) __ r T * 1 r r fi fl * 1 v r 1 _4 L— ................. ; ................................................................................................. .1 :_ ....... ‘ ......... ...................................................................................................... _: g ..................................................................................................... z: E 1 3 : : . Q 0 . . O . :1 b 1 1 1 1 1 1 1 Q 1 1 1 1 1 1 A l 1 1 1 1 1 1 1 d 0 0.0002 0.0004 0.0006 0.0008 0.001 0. 012 1,2-DCE-l Degradation Rate (day‘l) Figure 34. Sensitivity plots of model error (RMSE) of the mother/daughter ratios (PCE/TCE path) in response to varying degradation rates (model rate is circled). A) The aerobic 1,2-DCE rate in the shallow zone. B) The anaerobic 1,2-DCE rate in the middle zone (dashed line is where 1,2-DCE rate cannot be less than the VC rate in this zone). C) The anaerobic 1,2-DCE rate in the deep zone. 102 115 . . ~ 1 . - . 1 1 1 . - . >- ' :r :4 F : i 9 d 105 L11‘..‘_' ................................................................. .. ___: +— - ' -< +- ; : . . 1 A _y l‘ ' ‘ : : t j 95 _l ................ . .................. _ I g g t , , 3 85 _'_ _l. ....................................... _1 m : ? 3 . : , : CD " 3 :I r : : -1 7S ;......._--......_..: .................... :..._............-...in..-“.......-..._...:....1..-.-.....-._...:.. ................ _1 — f :| : : : 1 >— ‘ . ' , L :‘4 65 ;.,...-_....,11--.E....._........_....1......-......1-.....4:....-1....-...1..-1.1..1..........--.1..1.; .................. _.1 : E :l f O f : 3 55 L .................. ............... - .................... .................. .5 _ 1 I : : ; .1 e 1 - : : : n 45 ; ................. i ..................... ................... ; ..................... : ..................... .................. _-: : 3 :é E : : 3 35 * 1 1 1 i 1 1 R1 1 1 1 i 1 1 1 1 1 1 1 1 1 1 1 0 0.02 0.04 0.06 0.08 0.1 0.12 VC-2 Degradation Rate (day‘l) 45 . . Y 1 . v . I f . Y .I v r v 1 . v v i I i a 1 2 43 ._ ..... 1 .............. -.1 ..................... L ..... B 1-_( LL} 4] ;.. ................ 1 .................... ; .................... .I .................. _:. U) P i f : I I ‘ E 39 ; ....... , ......... .................... i. ......... . ......... ................. r, ................... I .................. S “ E E i E ' 1 t a s 5 s 1 ' : z : d 37 1...; ............ . ........ ............... . ..... ..................... ; ..................................... _1 35 l‘ 1 n 1 i 1 1 1 1 1 1 1 1 1 1 1 i 1 1 1 '1 1 1 1 A 0 0.00002 0.00004 0.00006 0.00008 0.0001 0.00012 VC-l Degradation Rate (day") 45 ‘ i * a I *fi 1 1 r T 1 r r _ I : 43 ._.' ........... . ......... ;-...-.._.-.-....-_11.: ....... ...............’ .......... . .......... L ..... ——4 : l E 1 2 C : 11.1 1. ; ................ I ......................................... . __________________ j m '- | - -1 5 ~ : = : 39 P ................. I ......... . ......... 3 ............................................................ z 37 L ....................................................................................................................... L C l , _ , . Z 35 1 1 i 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 J 1 1 1 0 0.0001 0.0002 0.0003 0.0004 0.0005 0.0006 VC-l Degradation Rate (day‘) Figure 35. Sensitivity plots of model error (RMSE) of the mother/daughter ratios (PCE/TCE path) in response to varying degradation rates (model rate is circled). A) The aerobic VC rate in the shallow zone (dashed line is literature value boundary). B) The anaerobic VC rate in the middle zone (dashed line indicates VC cannot be higher than deep zone). C) The anaerobic VC rate in the deep zone (dashed line represents boundary where the VC rate in the deep zone cannot be lower than the middle zone). 103 25 -.3.T.-.-,..Tfi....,..-.,..-.,fi--- 23 2T RMSE O O O 1 1 ‘ 1 v ' ‘ 1 . 1 1 1 . >- . . . 1 A A A A A A 11.1 111 11 1 0.0002 0.0003 0.0004 0.0005 0.0006 0.0007 TCA-B2 Degradation Rate (day") 25.13-fi }- -< " . ‘ i 1 i - -‘ . . 1 . . . »— 1 . , . 1 1 -< : I 1 - ' , 23 P ....................... , .......................................... ._ .................................... _1 >- ; ' .' 1 l l 4 r- . - 1 1 .1 ; . : . O 1 "' . - ~ 1 1 - —< ‘ I i . I I 21 __.1.11.......1.11.........1......1...........-.-...1 ...... . ....... ...3”......_......-..:.1..............;. .............. _. >— . 1 - = A .4 RMSE O *1 l— . . . . . . 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 l 1 1 1 1 l 1 1 1 1 1 0 0.0001 0.0002 0.0003 0.0004 0.0005 0.0006 0.0007 TCA-Bl Degradation Rate (day‘) 25 T T T Ta T T ' ' T ' ' ' T ' T ' Ta 7 T ' TV .4 ~ : u - 1 I "‘ 1 ~ 1 1 1 u r— . . 1 - 1 .1 . 1 1 u ' U , 1 1 1 ‘ ‘ ,_._.. .......... 1 .................................................. ., .......................................... _. . . 1 . 1 4 ‘ 1 1 1 I ’- ' . 1 . 1 I —4 1 . , 1 1 1 ‘ ‘ 1 . 1 _‘ -1 . . . 1 . >- ' ‘ 1 1 . . 21 .__ .................... . ......................... . ....... ;..... ....-.1...:..............-..; ............... ._1 . < ‘ 1 1 ‘ . - . 1 . 1 RMSE g4 11 '5 1i1111.11111111 0.0002 0.0004 0.0006 0.0008 0.00] 1 i . 1 1 i . 1 1 0.0012 0.0014 0.0016 TCA-Bl Degradation Rate (day“) Figure 36. Sensitivity plots of model error (RMSE) of the mother/daughter ratios (TCA path) in response to varying degradation rates (model rate is circled). A) The aerobic TCA rate in the shallow zone. B) The anaerobic TCA rate in the middle zone. C) The anaerobic TCA rate in the deep zone. 104 30 1— ‘ 1 r T fir fir * fir * # r T V E 5 2 275 E ...... .9 ......... ?' ......................................................................... A La 1 S 1 : a j 25 ,— .................. . ............................................................................................ _-: m C 3 a CD 2 ' I E 225 C“ .................................................................................................................. j i o : 20 L. ........................................ _‘1 " : 1 175 :_W ............................ T .......... ........................................ . ................. L i s 6) ° 5 3 15 P 1 g . i m L - 1 1 1 1 i m 1 . 1 1 1 1 D 0 0.002 0.004 0.006 0.008 0.01 0.012 DCA-2 Degradation Rate (day") 30 ’- fi 1 r * T T T T 1 1 T ' Y Y .. t j l 1 27.5 :_ ............................................................................................... I .......... 1 B k: — 1 25 :_ ............................................................................................. l.... ................. .3 a : . I : r 225 L ....... 9. ..................................................................................... 1....- .................. _Z 5 C ° : 20 :_ ............................................................ ................................... I ................ _: : 0 | 1 : 175 L .......................................... ........................................................... .2 15 ’ 1 1 l . i . 1 . i 4 1# i . . 1 1 1 1 " 0 0 .0002 0.0004 0.0006 0.0008 0.001 0.00 l 2 DCA-l Degradation Rate (day") 30 . - - - 1 . . . - 1 - - . . . . . . . I . . . - I . fi- 2 Z s a i g E 1 27.5 E— ------------------ f. .................... g .................... ...... C J 25 E ................. ,. .. ................. .1. m _ 1 m p 2 E 225 To" ......................................................................................................................... _. 1.9 1 20 7...... ..................................................................................................................... L 17.5 E_ .......... O. .......... 0. ........................................................................ f. ................. _: ._ J . O ‘ : Q : 3 l5 ” . z n i 1 1 1 1 1 1 1 1 1 . 1 . 1 1 . . 1 1 1 . A . " 0 0.001 0.002 0.003 0.004 0.005 0.006 DCA-1 Degradation Rate (day") Figure 37. Sensitivity plots of model error (RMSE) of the mother/daughter ratios (TCA path) in response to varying degradation rates (model rate is circled). A) The aerobic DCA rate in the shallow zone. B) The anaerobic DCA rate in the middle zone (dashed line indicates the rate in the middle zone cannot be higher than in the deep zone). C) The anaerobic DCA rate in the deep zone. 105 40 35 3O RMSE 25 20 16.5 RMSE RMSE Figure 38 Sensitivity plots of model error (RMSE) of the mother/daughter ratios (TCA path) in response to varying degradation rates (model rate is circled). A) The aerobic 1,1-DCE rate in the shallow zone. B) The anaerobic 1,1-DCE rate in the middle zone (dashed line indicates the 1,1-DCE rate cannot be lower than the VC rate in this zone). """" I ' ‘ ' ' ' T *—' Y I z T f .1 L .................................... g ........................................................... _. A .0; :0 i i :. ................................... - ........................................................... : ................. _J : 0 - V , _ ’ ___________________ é ................. : : 0 é : M 1 1 1 G '1 1 1 1 1 1 lllll 1 1 1 A 1 1 1 i ..... d 0 0 0012 0.0024 0.0030 0.0048 0.006 0.0072 11DCE-2 Degradation Rate (day") ' ' ' ' T ' fl ' r r V? I * fl 1 V _4 . ........................ I B .....1 ., ... . I ...................................................................... xi I , o 2 i _____________ _ _______________ _ ............................................................................ . I 1 1 E . . 1 1' 1 I. 1 1 . 1 1 1 1 1 . 1 1 1 . i . 1 #2 0 0.00007 0.000 14 0.00021 0.00028 0.00035 0.00042 1 1DCE-l Degradation Rate (day‘l) _ r fi m z r r T f r f * r fi' _‘ : . $ ‘ : l- : E -4 :- .................. 1....................: ............................................................. . .................. __: : ° 6 ° ° : :_ .................. ' ....................... ' .................................................................................. _.‘1 l- : '1 C ; j g. ............ ......................................................................................... i I E ' g ’— 1 1 1 i + 1 1 1 1 1 1 1 1 1 1 1 1 1 1 l 1 1 1 "l 0 0.0002 0.0004 0.0006 0.0008 0.001 0.0012 llDCE-l Degradation Rate (day") C) The anaerobic 1,1-DCE rate the deep zone. 106 zzvafiYVfivvvvuvv 1111111 21 E. .............................. I..-........... ...... A .1: 1 5 5 :I 5 5 o 3 20 L ............... .................. 1 .......... , .......... j. .................. ................ f ................... j I z 3 ;| s s : Lu ’ 3 Cl) 19 Ll .......................................................... .: E E g 3 : 18 :. .................. I ..................................................... .: E il 5 I7 :. ................... 1 ...................................... ................................ ... ........................ .5 16 1:. .................. .. é ....... ..., ................. .3 15 : 1 i 1 1 1 1 1 1 1 il 1 1 1 1 1 1 - l 1 - 1 : 0 0.014 0.028 0.042 0.050 0.07 0084 V02 Degradation Rate (day") 22 . . . r r . . I . . . . . . . . . . . - _ 2] P! ................................................................................................... I ...... B .: E l 3 20 T ..................................................................................................... _ .................. 1 : o I 2 531 19 :. ...................................................................................................... I. ................. .: E 18 a .............................................. 1 ................................................. 1 ................. .3 1 1 1 1 17 E. ......................................................................................................................... . 16 E. ........................................................................................................................ T: 15 : 1 1 1. 1 1 1 1 1 1 1 1 1 1 l 1 1 - ’ 1 1 1 Z 0 0.00002 0.00004 0.00006 0.00008 0.0001 0.00012 VC-l Degradation Rate (day") 27- ' ' ‘ ‘. ' " ‘ F ' ' ‘ I ' ' * 1 ' ' ' 1 ' ' - - 3 E E F E 1 2| T ........ I ........... ...... C .: I E I 3 s 2 5 : 20 “.----- ..... .................... g. .................... g. .................. _: E E I i g g g : m 19 - ................. .3 m t I j E 18 T ........................... I ............................................................................................ .: 17 f. ............................ I. ............................................................................................. .g E - o o o 9 3 16 E. ..................................................................................................................... .j 15 t 1 1 1 I1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 : 0 0.00007 0.00014 0.00021 0.00028 0.00035 0.00042 G VC-l Degradation Rate (day'l) Figure 39. Sensitivity plots of model error (RMSE) of the mother/daughter ratios (TCA path) in response to varying degradation rates (model rate is circled). A) The aerobic VC rate in the shallow zone (dashed line is literature value boundary). B) The anaerobic VC rate in the middle zone (dashed line indicates VC cannot be higher than deep zone). C) The anaerobic VC rate in the deep zone (dashed line represents boundary where the VC rate in the deep zone cannot be lower than the middle zone). 107 Discussion The simulated mass of PCB was lower than the estimated mass in each zone. The reason is that PCE is retarded more than the other compounds, and at the time the observed measurements were taken, the PCB plume was just arriving at the monitoring well transect. The retardation could be lowered to allow more mass to reach the transect, but the modeled PCE retardation factor was at the low end of the range of observed values in sandy aquifers. Also, increasing hydraulic conductivities caused the other species to travel too far downgradient. The higher observed mass may be due to small areas of preferential flow along which PCE traveled and reached the transect before the majority of the PCB plume arrived. Examination of the observed masses shows several trends that can be explained by the suspected redox conditions. The 1,2-DCE, DCA, and VC values are greatest in the deep zone. This can be attributed to two factors: recharge has forced the majority of the mass to the middle and deep zones and also that the degradation rates of TCE and TCA are greater in the deep anaerobic zone, which results in the production of more mass of the daughter products in the deep zone. Vinyl chloride is completely absent from the shallow zone, which may be due to the high aerobic degradation rate of VC in the shallow zone, which removes the VC from the system. VC is also absent from the middle zone, which may be the result of no VC production in this region because DCE does not readily degrade under denitrifying conditions (Chappelle, 1997). However, the middle zone is the problem area of the model, and using a very low degradation rate (105/day or lower) resulted in significantly much more mass in the middle zone. The problem may be that the conductivities in these zones are too high, therefore too much mass is moving 108 through these zones. The nature of numerical model results is that the solutions are non unique. However, estimating the degradation rates of plume G with the RT3D model was useful. The preliminary sensitivity simulations narrowed the range of reasonable rates to around 10'3 to 10‘4 day'l. Although a combination of other rates in this range may produce the same results, at the very minimum it has been shown that the natural degradation rates are rather low. This indicates that while natural attenuation is occurring at the site, it seems unlikely that it would be a viable treatment strategy for the entire plume since the degradation rates are so low. SIGNIFICANCE AND APPLICATIONS Novel Aspects of the Model Several aspects of the RT3D model were significant. The plume G reactions package is similar to the pre-defined sequential aerobic/anaerobic PCE/TCE dechlorination model predefined in RT3D (Clement, 1997) that was used at the Dover site by Clement et al. (2000). However, the model differs from Clement et. al. (2000) because it addresses TCA degradation in the same system as PCE/TCE degradation. The model also simultaneously describes abiotic and biotic transformation of TCA, which does not appear to have been examined in the modeling literature. Perhaps the most important aspect of the work was the calibration approach. Using the ratio of parent compound/daughter degradation byproduct as the comparison to calibrate the model was a new approach to reactive transport model calibration. The ratio approach to reactive transport calibration could be applied to any situation where source contaminants have 109 degraded to daughter byproducts. The approach focuses research on understanding other aspects of the system, such as degradation process, instead of concentrating on the source term problem. Applications of the Research to the Site The RT3D model that was created for plume G has several applications for research at the site. The model can be used to estimate remediation times for the compounds if monitored natural attenuation was the only strategy employed. Also, if an in situ system such as the plume A biocurtain is developed for plume G, then the natural attenuation rates could be coupled with a model that describes biostimulation or bioaugmentation to estimate a remediation time for the in-situ system. Both of the aforementioned applications could become part of a cost benefit analysis to compare the different remediation techniques available at the site, such as pump and treat, monitored natural attenuation, and in situ bioremediation. RECOMMENDATIONS FOR FUTURE WORK The results for the RT3D model were based on several assumptions and further research would help to determine if the assumptions were valid. Reducing the uncertainty associated with the advection and dispersion parameters of the model is an important task that could be easily addressed. Collection, analysis, and interpretation of a plume scale data set that includes redox analyses would be more costly and require more time, but may serve to reduce significant uncertainty associated with redox interpretations and subsequently the degradation rates. Lab analyses of degradation processes at the site 110 would serve to further support the rate estimations. Lastly, using an automated optimization scheme would quantify the model’s sensitivity to perturbations in the degradations rates and allow assessment of the uniqueness of an optimal solution. The hydraulic conductivity of the aquifer was represented by five different materials in the flow model, yet the retardation factors and porosity used in the reactive transport model did not reflect this heterogeneity. The porosity and sorption characteristics of the different materials were expected to be different. The porosity of the different materials could be determined from sieve analyses of the MSU 1-9 cores, while the sorption properties could be determined through batch reactions. The results are significant because the porosity affects the average linear velocity calculated by the advection equation and the sorption characteristics control the retardation factors of each species. The effect of one or both factors may significantly reduce or increase the travel time for solutes in the system, which may subsequently change the degradation rates estimated during the calibration. A plume scale geochemical dataset that includes redox data in addition to analysis for all compounds included in the RT3D reaction package equations is needed to further constrain the model. Redox analyses could be used to check the interpretations made in this thesis and to further delineate any other redox zones that may be present, such as a more reducing environment near the source as is typically observed at contaminant plumes (Azadpour-Keeley, et. al. 2001). Tracer normalization calculations to determine site-specific degradation rates could be performed using chloride data, which could be used to check the results of this work. The dataset could be used to estimate the total mass of each contaminant in the system, which provides another constraint on the 111 contaminant source term of the model. Lastly, collection of the plume scale geochemical dataset at multiple time periods (with about a year or so between each sampling event to see significant change in contaminant concentrations) would allow temporal comparisons of the model to observed data, which would serve to further reduce the uncertainty associated with the model results. Laboratory analyses of aquifer materials from the site would help support (or negate) a major assumption of the model. It was assumed that 1,1-DCE was formed solely as the result of abiotic degradation of TCA based on McCarty (1997). Lab analyses could determine if 1,1-DCE was being produced by abiotic TCA transformation, or if TCE degradation produced the significant amount of 1,1-DCE observed at the site. A side product of the tests would be degradation rates that could be compared to the field estimated rates. The analyses are significant because VC is a major concern at the site, and the bioremediation system that is designed would need to incorporate the TCA source of 1,1—DCE and subsequently VC if lab tests confirmed McCarty (1997). Automated calibration of the model using an optimization scheme would be beneficial to the study. An optimization code would greatly reduce the time needed to calibrate the model. The trial and error method was used, which was very time consuming. The optimization run would also quantify that the estimated degradation rates resulted in a minima in the objective function and could provide sensitivity parameters for the model inputs. 112 APPENDICES 113 APPENDIX A. WELL LOG DESCRIPTIONS FOR MSU WELLS 1-9 Well Log for MSU-1 Ground Elevation: 264.9 m Well drilled with a Hollow Stem Auger and aquifer sampled with Waterloo Cohesionless Sand Sampler Top Depth (milottom General Description 0 9.1 NO SAMPLE 9.1 12.2 very fine to fine sand 12.2 13.4 medium to coarse sand 13.4 13.7 NO SAMPLE 13.7 14.6 fine to medium sand 14.6 16.2 medium to coarse sand 16.2 16.5 NO SAMPLE 16.5 17.1 medium to coarse sand with some gravel 17.1 18.0 coarse sand with some gravel 18.0 18.3 fine sand 18.3 19.8 NO SAMPLE 19.8 25.0 coarse sand and gravel 25.0 25.3 clay Well Log for MSU-2 Ground Elevation: 265.1 m Well drilled with a Hollow Stem Auger and aquifer sampled with Waterloo Cohesionless Sand Sampler Top Depth (ml)30 t tom General Description 0 9.1 NO SAMPLE 9.1 12.2 very fine to fine sand 12.2 12.8 fine to medium sand 12.8 13.7 medium to coarse sand with some gravel 13.7 16.2 fine to medium sand 16.2 16.8 NO SAMPLE 16.8 17.7 medium sand 17.7 18.0 NO SAMPLE 18.0 24.7 coarse sand and gravel 24.7 25.0 clay Well Log for MSU-3 Ground Elevation: 265 m Well drilled with a Hollow Stem Auger and aquifer sampled with Waterloo Cohesionless Sand Sampler Top Depth (milottom General Description 0 9.1 NO SAMPLE 9.1 12.5 very fine to fine sand 12.5 13.1 medium to coarse sand with some gravel 13.1 13.4 NO SAMPLE 13.4 14.6 fine sand 14.6 18.3 medium to coarse sand with some gravel 18.3 25.0 coarse sand and gravel 25.0 25.3 clay 114 Well Log for MSU-4 Well drilled with a Hollow Stem Auger and aquifer sampled Ground Elevation: 264.9 m with Waterloo Cohesionless Sand Sampler Top Del“! ("1:30 t tom General Description 0 9.1 NO SAMPLE 9.1 12.2 very fine to fine sand 12.2 12.8 NO SAMPLE 12.8 14.6 medium to coarse sand 14.6 14.9 NO SAMPLE 14.9 15.2 fine to medium sand 15.2 18.0 medium to coarse sand 18.0 18.3 NO SAMPLE 18.3 23.8 medium to coarse sand with some gravel 23.8 24.7 coarse sand and gravel 24.7 25.3 clay Well Log for MSU-5 Ground Elevation: 265 m Well drilled with a Hollow Stem Auger and aquifer sampled with Waterloo Cohesionless Sand Sampler Top Depth (mEottom General Description 0 9.1 NO SAMPLE 9.1 13.7 very fine to fine sand 13.7 14.6 medium sand 14.6 18.3 medium to coarse sand with some gravel 18.3 19.8 NO SAMPLE 19.8 20.1 fine to medium gravel 20.1 20.7 medium to coarse sand with some gravel 20.7 21.3 NO SAMPLE 21.3 25.3 coarse sand and gravel 25.3 25.6 NO SAMPLE 25.6 25.9 Clay Well Log for MSU-6 Ground Elevation: 265.1 m Well drilled with a Hollow Stem Auger and aquifer sampled with Waterloo Cohesionless Sand Sampler Top Depth (ml)30ttom General Description 0 9.1 NO SAMPLE 9.1 12.2 fine sand 12.2 12.5 NO SAMPLE 12.5 13.1 medium to coarse sand with some gravel 13.1 13.7 medium sand 13.7 17.4 medium to coarse sand with some gravel 17.4 18.3 fine to medium sand with some gravel 18.3 22.3 medium to coarse sand with some gravel 22.3 25.0 coarse sand and gravel 25.0 25.3 clay 115 Well Log for MSU-7 Ground Elevation: 265.1 m Well drilled with a Hollow Stem Auger and aquifer sampled with Waterloo Cohesionless Sand Sampler Top Depth (mEottom General Description 0 9.1 NO SAMPLE 9.1 12.2 fine sand 12.2 13.1 medium to coarse sand 13.1 13.4 NO SAMPLE 13.4 13.7 fine sand 13.7 16.2 medium to coarse sand with some gravel 16.2 16.8 medium sand 16.8 18.6 NO SAMPLE 18.6 19.5 medium to coarse sand 19.5 19.8 NO SAMPLE 19.8 24.7 coarse sand and gravel 24.7 25.3 medium to coarse sand 25.3 25.6 fine to medium gravel 25.6 25.9 clay Well Log for MSU-8 Ground Elevation: 264.9 m Well drilled with a Hollow Stem Auger and aquifer sampled with Waterloo Cohesionless Sand Sampler Top Depth ("1:30 t tom General Description 0 9.1 NO SAMPLE 9.1 12.2 very fine to fine sand 12.2 13.1 coarse sand with some gravel 13.1 13.4 NO SAMPLE 13.4 13.7 fine to medium sand 13.7 16.8 medium to coarse sand 16.8 18.3 medium sand 18.3 27.1 coarse sand and gravel 27.1 27.4 gravel 27.4 27.7 clay Well Log for MSU-9 Ground Elevation: 265 m Well drilled with a Hollow Stem Auger and aquifer sampled with Waterloo Cohesionless Sand Sampler Top Depth (mgiottom General Description 0 9.1 NO SAMPLE 9.1 12.2 very fine to fine sand 12.2 13.1 medium sand 13.1 13.7 medium sand with some gravel 13.7 14.6 medium to coarse sand 14.6 18.3 medium to coarse sand with some gravel 18.3 22.9 NO SAMPLE 22.9 23.5 coarse sand and gravel 23.5 24.4 medium sand with some gravel 116 APPENDIX B 3-D SOLID STRATIGRAPHY MODELING IN GMS INTRODUCTION Appendix B was included to more fiilly explain the development of the 3-D solid objects in GMS. The methodology is explained by describing the steps used to create one of the 3-D solid objects. The solid that will be explained is depicted in Figure B-l, which shows the maximum extent in plan view and the 3-D object in relation to the cross section presented in Figure 22. The example is a solid that represents a portion of the aquifer that is composed of material 2, or fine to medium sands. The general progression started by creating boreholes from well log data, creating Triangular Interpolated Networks (TINS) from the Boreholes, and then creating Solids from the TINS. GMS BOREHOLE DATA ANALYSIS The well logs were digitized into a specific file format that was required by GMS before any work started. The process involved tabulating the X,Y,Z coordinates of the materials in a given borehole and listing them in descending order (please refer to the GMS manual (BYU, 2000) for further description of the Borehole file format). The borehole file was then imported into GMS. A plan view map showing the locations of the boreholes used is presented in Figure B-2. Note that there are several “dummy” wells located along the perimeter of the local model area. These wells were created and included so that irregular solid geometries would not be encountered along the margins of the grid. The lithology and thickness of the materials in the “dummy” wells were simply 117 determined from the NUS or MSU wells closest to them. The aquifer materials near plume G were based on observed data, thus the dummy wells had no effect on results. TRIANGULAR INTERPOLATED NETWORKS The first step required to make the TINS from the boreholes was to define a boundary to contain the extrapolated TIN S. A boundary was created that was slightly larger than the local model grid (Figure B-2). Two TINS were needed to make a given solid; one TIN was needed to represent the top surface of the material and one TIN was needed to represent the bottom surface of the material. For the example, the top tin was created by selecting the contact of material 1 and material 2 in the appropriate boreholes and then using the CONTACTS to TIN command of GMS. The TIN that is created extends outward from the selected boreholes until it intersects the boundary polygon and it is truncated midway between adjacent boreholes where no contact is selected. The lower TIN was created in a similar manner, except that the nodes interior to the model along the edge were moved to make it slightly larger than the top TIN (the reason is explained later in the CREATION OF 3-D SOLID OBJECTS section). The top and bottom TINS are shown in Figures B-3A and B-3B respectively with the boreholes used to create them. The interior edge nodes of the top TIN were then snapped to the lower TIN, which pinched out the material at the edge (Figure B-3C). CREATION OF 3-D SOLID OBJECTS The top and bottom TINS for the example were selected and the FILL BETWEEN TINS to SOLIDS command was used to create the solid. GMS creates the solid by filling 118 downward from the top TIN until it intersects the lower TIN. If the lower TIN is smaller than the top TIN, GMS will extrapolate far below the bottom TIN, creating an erroneous solid. This was the sole reason for modifying the bottom TIN to make it slightly larger than the top TIN. The solid was then complete, and was assigned appropriate material properties as described in chapter HI (Figure B-3D). All of the other solids were created in the exact same manner as just described. 119 l MATERIAL KEY I - Material 1 — Very Fine to Fine Sand - Material 2 — Fine to Medium Sands - Material 3 — Coarse Sands - Material 4 — Medium to Coarse Sands some Gravel - Material 5 — Coarse Sands, Gravels, and Pebbles Figure B-l. Location of the solid for which an explanation of 3-D solid construction in GMS is presented in Appendix B. The inset shows the areal extent of the solid with respect to the local model grid and in reference to the cross-sections. Image is presented in color (V E = 20X). 120 \ 1.; A A A ‘ ‘ A A A A “ , e‘ \ \ ‘ ‘ ‘ \. A NUS Monitoring Well I MSU Monitoring Well . “Dummy” Well LEGEND E2] Local Model Grid 1:] TIN Boundary Polygon O 800 5: meters Figure B-2. Location of the wells used to create the TINS and solids in GMS. 121 D l MATERIAL KEY I Material 1 — Very Fine to Fine Sand Material 2 — Fine to Medium Sands Material 3 — Coarse Sands Material 4 — Medium to Coarse Sands some Gravel Material 5 — Coarse Sands, Gravels, and Pebbles Figure B-3. Generalized steps of solid object construction from a set of borehole objects in GMS. A) Creation of a TIN representing the top of a solid. B) Creation of a TIN representing the bottom of a solid. 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