.,.,, : lin‘ . ...o .2 x. . . .(w‘ .5333. an. 3 flagfin ..s 3... 11th... . :5. a... . .. v2.2 Re: L 0““... a? be ~ é: . .3 an“. v .fi 3:: . x 6.? . :5... r. .u 9*... J. rt... v u 3/. .3... 1 ...« . may 83%? start ‘LI‘UV E...) w or u 3...": £3.95 aubmmdm..hx. . : Mummy“?! ...... 5%.: «no... u“ $5: --~‘“ Er , . k knsumlzéx. . A...“ 7‘ , H” . .5 x , . .. a; . ‘ . «32m. ”it rt: a «.th n2- rikwma. xv. 1%... .awnri r » ..AI.1..«". 5: t 8... I. .I. J. . .91....“ a»: .53.": {A :35. 5.: s... . a my .2. » ,5...5.3.3 .2. nifima .. V nsnspunfl Z. ‘.L 411:5. . . 1212.518 300$ LIBRARY Michigan State URIVGI sity This is to certify that the dissertation entitled WOOD-CEMENT PARTICLEBOARD: IMPROVED MANUFACTURING, MATERIAL CHARACTERIZATION AND POTENTIAL APPLICATION IN CONCRETE CRASH BARRIERS presented by AN GONG has been accepted towards fulfillment of the requirements for the PhD. degree in Civil ErLgineerinL 7.7 ' J/“i/ng'VW , Major Professor’s Signature %}(LAZ(1 27L 026,05. Date MSU is an Affirmative Action/Equal Opportunity Institution PLACE IN RETURN BOX to remove this checkout from your record. T O AVOID FINES return on or before date due. MAY BE RECALLED with earlier due date if requested. DATE DUE DATE DUE DATE DUE 2/05 WW“ WOOD-CEMENT PARTICLEBOARD: IMPROVED MANUFACTURING, MATERIAL CHARACTERIZATION AND POTENTIAL APPLICATION IN CONCRETE CRASH BARRIERS By An Gong A DISSERTATION Submitted to Michigan State University in partial fulfillment of the requirements for the degree of DOCTOR OF PHILOSOPHY Department of Civil and Environmental Engineering 2005 ABSTRACT WOOD-CEMENT PARTICLEBOARD: IMPROVED MANUFACTURING MATERIAL CHARACTERIZATION, AND POTENTIAL APPLICATION IN CONCRETE CRASH BARRIERS By An Gong Recycling waste wood into wood composite products is increasingly attractive to reduce environmental problems associated with disposal and promote sustainable development. For use in engineering applications, in addition to developing suitable manufacturing methods, the material and load bearing characteristics of wood-cement particle composites must be thoroughly investigated. This research focuses on wood-cement particleboard (WCPB). An improved manufacturing process that yields superior wood-cement particleboard is developed; material properties required for engineering design are experimentally determined; and the potential application of wood-cement particleboard to enhance the impact characteristics of concrete highway crash barriers is investigated. A pressure controlled, fully saturated curing process is developed to enhance the bond between wood particles and the cement matrix to produce a superior wood-cement particleboard. The bending, compressive and impact characteristics of wood-cement particleboard produced using this process are experimentally determined. The optimum cement/wood ratio also is determined. The experimental results indicate that WCPB is able to absorb a significant amount of energy by undergoing large nonlinear deformations. With the aim of taking advantage of its energy absorbing capability, the potential application of WCPB to enhance the impact characteristics of concrete highway crash barriers is investigated. Computational simulation is performed using the LS-DYNA finite element analysis code. The FE simulation agrees reasonably well with impact test results obtained in the laboratory. This suggests that the LS-DYNA material models can be effectively applied to model concrete and wood-cement particleboard. Subsequently, vehicle crash simulations are performed on a concrete crash barrier and a concrete crash barrier with WCPB facades to determine whether WCPB can enhance the impact characteristics. It is found that a flat WCPB facade is too stifl‘ relative to the flexibility of the vehicle bumper system and does not yield a significant reduction in the impact deceleration force on the vehicle. However, a tubular facade made of WCPB yields reasonable reductions in impact force. A triple tube facade appears to yield the best impact characteristics, assures controllable deformations and provides optimal safety to the vehicle occupants. To my mother iv ACKNOWLEGEMENTS The author would like to thank Professors Ronald Harichandran and Pascal Kamdem for their academic guidance and financial support in seeing the project through to completion. The author would like to thank Professors Rigoberto Burguefio, Zhengfang Zhou and Parviz Soroushian for their academic guidance. Thanks also to Siavosh Ravanbakhsh for his support in laboratory experiments. TABLE OF CONTENTS LIST OF TABLES ..................................................................................................... x LIST OF FIGURES .................................................................................................. xii CHAPTER] OVERVIEW AND RESEARCH OBJECTIVES ...................... 1 1.1 Wood-Cement Particle CompOSItesl 1.2 Concrete Barners3 1.3 Research Objectives ........................................................................ 4 CHAPTER 2 INRODUCTION AND LITERATURE REVIEW ....................... 5 2.1 Introduction ..................................................................................................... 5 2.2 History and Development of Wood-Cement Composites ................................ 5 2.3 Environmental Risk of CCA Treated Wood ................................................ 7 2.4 Wood and Cement ........................................................................................... 10 2.4.1 Wood .......................................................................................................... 10 2.4.2 Cement .......................................................................................................... 16 2.4.3 Wood cement compatibility ........................................................................ 17 2.5 Bending Strength of Wood-Cement Particleboard ....................................... 19 2.5.1 Elasto plastic behavior .................................................................................. 19 2.5.2 Effect of cement to wood ratio ................................................................... 22 2.5.3 Effect of manufacturing method on strength ........................................... 23 2.6 Compressive Strength of Wood-Cement Particleboard ........................................ 24 2.7 Durability ....................................................................................................... 26 2.8 Insulation Properties .................................................................................. 29 2.8.1 Thermal properties .................................................................................. 29 2.8.2 Acoustic properties .................................................................................. 30 2.8.3 Fire resistance ........................................................................................ 30 2.9 Theoretical Studies ...................................................................................... 31 2.10 Applications of Wood-Cement Composites ................................................ 33 2.11 Highway Barriers .................................................................. 38 2.11.1 Introduction ...................................................................... 38 2.11.2 Barrier safety data ................................................................................. 40 2.11.3 Crash performance of concrete barriers ..................................................... 41 2.12 Concrete Material Model ................................................................................ 44 2.12.1 Biaxial and triaxial behavior .................................................................. 45 2.12.2 Characteristics of yield surface ...................................................................... 49 vi 2.12.3 Failure surfaces of concrete under different stress states .................... 50 2.12.4 Evolution of yield surface of concrete under muti-dimensional loading ........................................................................................................... 55 2.13 Finite Element Modeling for Vehicle Crash ........................................................ 56 2.13.1 Brief summary of formulation ..................................................................... 57 2. 13.2 Time integration ............................................................................................ 58 2.13.3 Contact algorithm .......................................................................................... 58 2.13.4 Force and displacement field quantities ........................................................ 59 2.13.5 Simulations of barrier crash tests using LS-DYNA ..................................... 59 CHAPTER3 IMPROVED MANUFACTURING PROCESS AND FLEXTURAL PERFORMANCE ...................................................... 62 3.1 Introduction ................................................................................. 62 3.2 Pressure Controlled and Fully Saturated Curing Process .......................... 63 3.2.1 Advantages of pressure controlled and fully saturated curing process .............................................................................. 63 3.2.2 Materials ............................................................................ 64 3.2.3 Manufacturing particleboard ............................................... 66 3.3 Flexural Properties of Wood-Cement Particleboard ............................... 69 3.3.1 Experimental design ................................................................. 69 3.3.2 Description of test ................................................................ 69 3.3.3 Test results and analysis ........................................................... 71 3.4 Discussion .............................................................................. 84 CHAPTER 4 COMPRESSIVE BEHAVIOR OF WOOD-CEMENT PARTICLEBOARD .......................................................... 86 4.1 Introduction .......................................................................... 86 4.2 Experimental Design ................................................................. 87 4.3 Compression Test ........................................................................ 88 4.3.1 Test method ......................................................................... 88 4.3.2 Failure modes ................................................................. 90 4.3.3 Compressive strength and stiffness .............................................. 94 4.3.4 Toughness .......................................................................... 98 4.4 Summary ................................................................................ 103 CHAPTER 5 IMPACT TESTS ON WOOD-CEMENT PARTICLEBOARD. . ..105 5.1 Introduction ....................................................................... 105 5.2 Falling Ball Impact Test ......................................................... 106 5.2.1 Impact test design ............................................................. 106 5.2.2 Design of impact test device ...................................................... 107 vii 5.2.3 Impact data recording devices ............................................. 110 5.2.4 Impact test setup .............................................................. 111 5.3 Multi-Stress Test on Wood-Cement Particle Tube ................................. 120 5.3.1 Test results and analysis ..................................................... 121 5.4 Summary ................................................................................ 125 CHAPTER 6 VALIDATION OF MATERIAL MODEL FOR WOOD-CEMENT PARTICLEBOARD ............................... 126 6.1 Introduction ......................................................................... 126 6.2 Finite Element Modeling of Falling Ball Impact Test ............................ 126 6.2.1 Modeling software ................................................................ 126 6.2.2 Element modeling ................................................................... 127 6.2.3 Material modeling ................................................................. 127 6.2.3.1 Modeling concrete ......................................................... 127 6.2.3.2 Modeling wood-cement particleboard ................................... 131 6.2.3.3 Modeling steel ................................................................. 135 6.2.4 Contact modeling ................................................................. 135 6.2.5 Boundary conditions ............................................................ 136 6.2.6 Database output node .............................................................. 137 6.2.7 Impact simulation and results ................................................. 137 6.3 Finite Element Modeling of Multi-Stress Test ..................................... 142 6.3.1 Element modeling ............................................................... 142 6.3.2 Material modeling ................................................................ 143 6.3.3 Contact modeling ................................................................ 143 6.3.4 Boundary conditions ............................................................. 144 6.3.5 Database output node ....................................................... 145 6.3.6 Multi-stress test simulation ...................................................... 145 6.4 Summary ............................................................................. 147 CHAPTER 7 FINITE ELEMENT SIMULATION OF VEHICLE CRASHING ON CONCRETE BARRIER ENHANCED WITH WCPB ................................................................ 148 7.1 Introduction ............................................................................. 148 7.2 Simulation Test Design and Evaluation Criteria ................................. 149 7.2.1 Concrete barrier .................................................................. 149 7.2.2 Enhanced concrete barrier ......................................................... 150 7.2.3 Simulation matrix ............................................................. 151 7.2.4 Evaluation conditions and criteria ............................................. 152 7.3 Finite Element Modeling ........................................................... 152 7.3.1 Element modeling ............................................................ 153 7.3.2 Material modeling ............................................................ 154 viii 7.3.2.1 Modeling concrete ......................................................... 154 7.3.2.2 Modeling wood-cement particleboard .................................... 155 7.3.2.3 Modeling steel ................................................................. 155 7.3.3 Contact modeling .................................................................. 156 7.3.4 Vehicle model ....................................................................... 157 7.3.5 Center of gravity of the vehicle .................................................. 157 7.3.6 Boundary conditions ........................................................ 158 7.4 Finite Element Simulation ............................................................. 159 7.4.1 Frontal crash simulation setup ................................................. 160 7.4.2 Simulation results .................................................................... 163 7.4.3 Comparison of WCPB, concrete and steel triple-tube facades .............. 176 7.5 Summary ................................................................................... 180 CHAPTER 8 CONCLUSIONS AND RECOMMENDATIONS FOR FUTURE RESEARCH ..................................................... 181 8.1 Introduction ............................................................................... 181 8.2 Development of wood-cement particle composites .................................. 181 8.2.1 Manufacturing process .......................................................... 181 8.2.2 Effect Of cement/wood ratio on bending strength .............................. 182 8.2.3 Compressive properties ............................................................ 182 8.2.4 Impact Characteristics .................................................... 183 8.3 Computational simulation for the application of wood-cement composites ............................................................................... 184 8.4 Future research ............................................................................ 185 APPENDICES ................................................................................... 186 Appendix A An 820C vehicle impacting a concrete barrier enhanced with a 3-tube wood-cement composite panel .......................... 187 Appendix B A steel ball impacting wood cement particleboard overlaying a concrete block ......................................................... 199 BIBLIOGRAPHY ........................................................................... 204 ix Table 2.1 Table 2.2 Table 2.3 Table 2.4 Table 2.5 Table 2.6 Table 3.1 Table 3.2 Table 3.3 Table 4.1 Table 4.2 Table 4.3 Table 4.4 Table 5.1 Table 6.1 Table 6.2 Table 6.3 LIST OF TABLES Industrial Production of Inorganic-Bonded Wood Composites ................ 6 Area of Forestland in the World by Geographic Location and Species Group 1980 ............................................................................ 11 Elemental composition of wood .......................................... 11 Organic Constituents of Wood ................................................... 12 Differences between hardwood and softwood .............................. 12 Rate of crash death on vehicle-barrier crash ..................... 41 Test Matrix for Bending Test ....................................................... 69 Flexural Performance of Wood-Cement Particleboard Subjected to Seven Different Cement/Wood Ratios ............................................ 75 Flexural Toughness of Wood-Cement Particleboard ........................... 80 Test Matrix for Compression on Specimens .................................... 87 Compressive Strength and Strain at Peaks stress for WCPB and Normal Concrete ............................................................................... 97 Stiffness of Wood-Cement Particleboard .................................. 98 Compressive Toughness of Wood-Cement Particleboard ................. 99 Test Matrix for Impact Test ..................................................... 107 Equation of State Algorithm for Generic Concrete ........................... 129 Concrete Material Parameters .................................................. 130 WCPB Material Data ............................................................ 134 Table 6.4 Table 7.1 Table 7.2 Table 7.3 Table 7.4 Material Data for Steel Ball ................................................... 135 Simulation Matrixes for Frontal Crash Impact ................................. 151 Concrete Material Parameters .................................................... 154 WCPB Material Data ............................................................... 155 Steel Bar Material Data ............................................................ 156 xi Figure 2.1 Figure 2.2 Figure 2.3 Figure 2.4 Figure 2.5 Figure 2.6 Figure 2.7 Figure 2.8 Figure 2.9 Figure 2.10 Figure 2.11 Figure 2.12 Figure 2.13 Figure 2.14 Figure 2.15 LIST OF FIGURES Softwood: Sitka sprue (x 75) ............................................................... 13 Hardwood: Red oak (x 50) .................................................................... 13 Most common forms of wood composites elements ................................. 14 Element of a knife-ring flaker ................................................................... 15 Main component and plates of disk refiner ........................................ 16 Typical load-deformation curve of wood-cement particleboard under bending ...................................................................................................... 20 F lexural stress vs. deflection curves under flexure for WCPC with normal and accelerated curing ................................................................... 21 Variation of MOR with cement-wood ratio ................................ 23 Compressive strength vs. wood/cement ratio ........................................... 25 Compressive load vs. deformation ...................................................... 26 F lexural strength vs. deflection under wetting and drying ........................ 28 F lexural strength vs. deflection under freezing and thawing .................. 28 Schematic representation of cracking through a fiber reinforced matrix ......................................................................................................... 32 Siding with WCPB in Japan ..................................................................... 33 Siding with WWCB in the Phillipines ............................................ 34 xii Figure 2.16a Figure 2.16b Figure 2.17 Figure 2.18 Figure 2.19 Figure 2.20 Figure 2.21 Figure 2.22 Figure 2.23 Figure 2.24 Figure 2.25 Figure 2.26 Figure 2.27 Figure 2.28 Figure 2.29 Figure 2.30 Figure 2.31 Figure 2.32 Figure 2.33 WCP block for building walls ................................................................... 35 Exterior and interior walls with WCP block .............................................. 35 Sound barrier of wood-cement particleboard (Czech Republic) ............... 36 Wood wool cement board for roofing and walls in Phillippines ............... 36 Wood strand cement board for all walls and sidings in Japan ................... 37 Roof decking with wood excelsior cement composites ....................... 37 Exterior-wall cladding of the Sandoz AG Laboratory in Basel, Switzerland ................................................................................................ 38 Flexible cable barrier ................................................................................ 39 Simi-rigid guardrail .................................................................................... 39 Rigid concrete barrier ................................................................................ 40 Major shapes of concrete barriers ........................................................... 42 Geometry of concrete barrier ..................................................................... 43 Demonstration of field test (top view) ....................................................... 43 Biaxial strength envelope of concrete ...................................... 46 Envelope of elastic limit and maximum strength of concrete ................ 47 Behavior of concrete in hydrostatic compression test ............................... 48 Schematic representation of the elastic limits and failure surface of concrete .................................................................................................... 49 Geometric representation of the stress state in the principal stress space ........................................................................................................... 50 Meridian and deviatoric sections for two parameter failure models .......... 52 xiii Figure 2.34 Figure 2.35 Figure 2.36 Figure 2.37 Figure 2.38 Figure 2.39 Figure 3.1 Figure 3.2 Figure 3.3 Figure 3.4 Figure 3.5 Figure 3.6 Figure 3.7 Figure 3.8 Figure 3.9 Figure 3.10 Figure 3.11 Figure 3.12 Figure 3.13 Figure 3.14 Figure 3.15 Hsieh-Ting-Chen criterion ......................................................................... 54 Evolution of concrete yield surface as proposed by Chen and Han .......... 56 Crash field test (fiont view) ...................................................................... 60 Crash Simulation (front view) ................................................................... 60 Crash field test (plan view) ........................................................................ 61 Crash simulation (plan View) .................................................................... 61 CCA-treated wood .................................................................................... 65 Wood particles ........................................................................................... 65 Wood particle cutting machine ................................................................. 65 Wood particle screener .............................................................................. 65 Cement wood particle mixer ...................................................................... 67 Hydraulic press .......................................................................................... 67 Curing in water ......................................................................................... 67 Saw used to cut board ................................................................................ 67 Flowchart of manufacturing process .......................................................... 68 INSTRON machine ................................................................................... 70 Bending test setup ................................................................................... 70 Specimen’s size .......................................................................................... 70 Bending failure ........................................................................................... 72 Cross-section view of failure .................................................................. 72 Load-deflection curves for varying cement/wood ratios ...................... 73 xiv Figure 3.15 Figure 3.16 Figure 3.17 Figure 3.18 Fihure 3.19 Figure 3.20 Figure 3.21 Figure 3.22 Figure 3.23 Figure 3.24 Figure 3.25 Figure 4.1 Figure 4.2 Figure 4.3 Figure 4.4 Figure 4.5 Figure 4.6 Figure 4.7 Figure 4.8 Load-deflection curves for varying cement/wood ratios ...................... 73 Correlation between MOR and cement/wood ratio .................................. 76 Correlation between MOE and cement/wood ratio ................................... 76 Correlation between density and cement/wood ratio ................................. 77 Toughness calculation curve (load vs. disp) ............................................ 79 Variation of modulus of rupture vs. cement/wood ratio (95%confidence) .................................................................................... 8 1 Variation of modulus of elasticity vs. cement/wood ratio (95% confidence) ...................................................................................... 82 Modulus of elasticity vs. cement/wood ratio ............................................. 82 Variation of density vs. cement/wood ratio (95% confidence) ....................................................................................... 83 Density vs. cement/wood ratio ................................................................... 83 Toughness index vs. cement/wood ratio (95% confidence) ...................... 84 Short column specimens ............................................................................ 87 Loading directions .................................................................................... 88 Compression speciemens ........................................................................... 89 Compression test set-up on INSTRON test machine ................................. 89 Failure modes (h/d=2.0, cement/wood ratio = 1.5) ................................... 91 Failure modes (h/d =20, cement/wood ratio = 1.0) .................................. 92 Failure modes (h/d =3.0, cement/wood ratio = 1.5) .................................. 93 Load-deformation curves (h/d=2.0, cement/wood ratio = 1.5) .................. 94 XV Figure 4.9 Figure 4.10 Figure 4.11 Figure 4.12 Figure 4.13 Figure 4.14 Figure 4.15 Figure 4.16 Figure 5.1 Figure 5.2 Figure 5.3 Figure 5.4 Figure 5.5 Figure 5.6 Figure 5.7 Figure 5.8 Figure 5.9 Figure 5.10 Load deformation curves (h/d =2.0, cement/wood ratio = 1.0) ................. 95 Load deformation curves (h/d =3.0, cement/wood ratio = 1.5) ................. 95 Stress-strain relationships of the wood-cement composite short columns .................................................................................................... 100 Compressive strength vs. cement/wood ratio (parallel loading) ............. 101 Compressive strength vs. cement/wood ratio (perpendicular loading) .................................................................................................... 101 Compressive stiffness vs. cement/wood ratio (parallel loading) .......... 102 Compressive stiffness vs. cement/wood ratio (perpendicular loading) .................................................................................................... 102 Compressive toughness index vs. cement/wood ratio ........................... 103 Schematics of impact test ..................................................................... 107 Release mechanism ................................................................................ 108 Schematic of the impact ball .................................................................... 109 Photographs of impact ball assembly .................................................. 109 353312 accelerometer ............................................................................. 110 Oscilloscope ............................................................................................. 110 Impact test setup .................................................................................... 111 Permanent deformations in wood-cement particleboard following impact ....................................................................................................... 112 Voltage vs. time (concrete) .................................................................. 113 Voltage vs. time (WCPB on concrete) .................................................. 113 xvi Figure 5.11 Figure 5.12 Figure 5.13 Figure 5.14 Figure 5.15 Figure 5.16 Figure 5.17 Figure 5.18 Figure 5.19 Figure 5.20 Figure 5.21 Figure 5.22 Figure 6.1 Figure 6.2 Figure 6.3 Figure 6.4 Figure 6.5 Figure 6.6 Figure 6.7 Figure 6.8 Voltage vs. time (wood on concrete) .................................................. 114 Acceleration time histories of steel ball (WCPB on concrete) .............. 115 Velocity time histories of steel ball (WCPB on concrete) ....................... 116 Displacement time histories of steel ball (W CPB on concrete) ............... 117 Acceleration time histories of steel ball (concrete, wood, WCPB) ......... 118 Velocity time histories of steel ball (concrete, wood, WCPB) ................ 119 Displacement time histories of steel ball (concrete, wood, WCPB) ........ 120 Geometry of speciemen .......................................................................... 121 Compression test setup ............................................................................ 122 Compressive failure of WCPB ring ......................................................... 123 Load-displacement curve for multi-stress test on WCPB ring ............... 123 Stress state and stress distribution ............................................................ 124 Hydrostatic stress vs. volumetric strain of concrete ................................ 128 Yield stress vs. mean stress for concrete under hydrostatic compression ............................................................................................. 130 Effective stress vs. effective plastic strain curve ..................................... 132 Engineering stress vs. engineering strain (W CPB) ................................. 133 Effective stress vs.effective plastic strain (WCPB) ................................ 134 FE model and boundary conditions ...................................................... 136 Output node location .............................................................................. 137 Finite element models .............................................................................. 138 xvii Figure 6.9 Figure 6.10 Figure 6.11 Figure 6.12 Figure 6.13 Figure 6.14 Figure 6.15 Figure 6.16 Figure 6.17 Figure 7.1 Figure 7.2 Figure 7.3 Figure 7.4 Figure 7.5 Figure 7.6 Figure 7.7 Figure 7.8 Figure 7.9 Figure 7.10 Figure 7.11 Acceleration time histories fi'om impact test and simulation (concrete) ................................................................................................. 140 Acceleration time histories from impact test and simulation (WCPB)....141 Velocity time histories from impact test and simulation ......................... 141 Displacement time histories from impact test and simulation ................. 142 Boundary conditions ............................................................................... 143 Location of output node ........................................................................... 144 Finite element model ................................................................................ 145 Deformed FE mode] ................................................................................. 146 Load—displacement curves from test and simulation ...................... 147 Geometry of the concrete barrier and steel reinforcement ................ 149 Enhanced vertical concrete barrier ........................................... 150 Cross section of particleboard panels ........................................ 151 Concrete and steel bar elements ................................................ 153 WCPB and concrete elements .................................................. 153 Mesh of steel reinforcement with beam element .......................... 154 1975 Honda Civic (820C) ...................................................... 157 CG and accelerometer location ................................................. 158 Boundary conditions of the FE model ...................................... 159 Vehicle crashing on concrete barrier ........................................... 160 Concrete barrier enhanced with flat WCPB facade ........................ 161 xviii Figure 7.12 Figure 7.13 Figure 7.14 Figure 7.15 Figure 7.16 Figure 7.17 Figure 7.18 Figure 7.19 Figure 7.20 Figure 7.21 Figure 7.22 Figure 7.23 Figure 7.24 Figure 7.25 Figure 7.26 Figure 7.27 Figure 7.28 Figure 7.29 Figure 7.30 Figure 7.31 Concrete barrier enhanced with double-wave WCPB facade .......... 161 Concrete barrier enhanced with triple-wave WCPB facade .............. 162 Concrete barrier enhanced with triple-tube WCPB facade ................. 162 Concrete barrier enhanced with four-tube WCPB facade .................. 163 Crash on concrete barrier ........................................................ 165 Crash on flat facade .......................................................... 165 Crash on double-wave facade .................................................................. 166 Crash on triple-wave facade ................................................................... 166 Crash on triple-tube facade .................................................................. 167 Crash on four-tube facade ........................................................................ 167 Vehicle damage after crash on concrete barrier (at t=70 ms) ................. 168 Vehicle damage after crash on flat WCPB facade (at t=7 0 ms) .............. 168 Vehicle damage after crash on double-wave WCPB facade (at t=70 ms) .............................................................................................. 169 Vehicle damage after carsh on triple-wave WCPB facade (at t=70 ms)..169 Vehicle damage after carsh on triple-tube WCPB facade (at t=70 ms)...170 Vehicle damage after crash on four-tube WCPB facade (at t=7O ms). . .170 Displacement time histories of vehicle ...................................... 172 Velocity time histories of vehicle ............................................. 172 Acceleration time histories of vehicle ......................................... 173 Deformation of triple-tube facade ............................................. 175 xix Figure 7.32 Figure 7.33 Figure 7.34 Figure 7.35 Figure 7.36 Vehicle crashing on WCPB triple-tube facade ............................... 177 Vehicle crashing on concrete triple-tube facade ......................... 177 Vehicle crashing on 3mm thick steel triple-tube facade ................ 178 Vehicle crashing on 5 mm thick steel triple-tube facade ................ 178 Acceleration time histories of vehicle for four triple-tube facades...l79 XX CHAPTER 1 OVERVIEW AND RESEARCH OBJECTIVES 1.1 Wood-Cement Particleboard Wood-cement particleboard is composed of wood particles, Portland cement (Type I) and water. Besides having higher material strength, good plasticity, good durability and better energy dissipation properties, it also has low cost, is lightweight and simple to manufacture (Kurfiel, 1995; Wolfe, 1996). It has been shown in practice that the wood-cement particleboard has advantages over conventional wood composites. At present, approximately 10,000 cubic meters of treated wood are removed from service in the United States and Canada every year. This figure is expected to increase in the next decade (Copper, 1993). However, only a small part of this large amount of waste wood is recycled into products, and most of the waste wood is discarded producing a negative effect on the environment. Therefore, recycling waste into wood composite products is highly beneficial. The tensile strength of wood-cement particleboard (WCPB) is about 3 times higher than normal concrete (Won, 1995, Moslemi and Pfister, 1987) and the compressive strength of WCPB is comparable to that of normal concrete (Blankenhor, 1994; Sorfa, 1984) Because WCPB has high porosity due to the presence of soft wood particles, it is capable of dissipating much more energy than concrete. The first toughness index of 1 WCPB for both bending and compression is six times higher than normal concrete (Wolfe, 1996) WCPB has advantages over conventional resin-bonded wood particle composites with respect to durability and fire resistance. WCPB meets the requirements for fire resistance and durability for outdoor applications (Wolfe, 1999). However, conventional resin-bonded wood particle composites do not meet the requirements of outdoor applications for either durability or fire resistance. Because WCPB is mainly made from waste wood removed from service, there is no cost for acquiring the raw material, and the manufacturing process for WCPB is quite simple. Use of waste wood to produce WCPB is environmentally fiiendly and beneficial to society. Even though WCPB technology was introduced about 40 years ago, it has not been rigorously investigated, especially in North America (Moslemi, 1989). As the use of WCPB material increases in The United States, more effort is being directed to research. Recent studies (Won, 1995; Wolfe, 1999; Zhou and Karndem, 2000; Horne, 1997) on wood cement particle composites have focused on manufacturing methods, material properties, durability and potential applications in engineering. The manufacturing method can significantly impact the material properties of wood-cement particleboards. The development of improved methods that yield WCPB with higher strength and stifliiess and reduce variability in material properties would be beneficial. With the increasing applications of wood-cement particleboard in construction 2 purposes, more and more research has focused on the study of the strength of the composite material and the effect of the cement/wood ratio on its material strength (Zhou and Kamdem, 2000; Eltomation, 2003). Perhaps of most relevance is the development of new high volume applications for the large amount of waste wood that is generated in the US. Successful applications of using wood-cement particle composites as exterior walls in houses (Home, 1997) and as sound barriers on highways (Wolfe, 1999) have begun a potential bright future for the application of this material in engineering. At present, WCPB products have been widely used in construction engineering as both structural and nonstructural members (Kurpiel, 1995; Home, 1997). Because WCPB has energy dissipating properties, it could also have special applications in structures where impact and dynamic load are a design consideration (Wolfe, 1999). 1.2 Concrete Crash Barriers Highway engineers are facing a significant challenge to improve the impact characteristics of concrete crash barriers to make the roads safer. Concrete crash barriers are used in the longitudinal direction of roads. Because the deflection of concrete barriers during impact is very small, the impact deceleration forces on vehicles impacting them are much higher than those on vehicles impacting other kinds of barriers such as guardrails. Therefore, enhancements to concrete barriers that reduce deceleration forces on impacting vehicles are highly desirable to improve safety for vehicle occupants. 3 1.3 Research Objectives The objectives of this research are to: Develop a new manufacturing method to improve the engineering properties of wood-cement particleboard. Characterize the response of WCPB under bending, compressive and impact loads. Assess the applicability of material models available in the LS-DYNA finite element package to simulate impact on WCPB. Use finite element simulations to investigate the feasibility of using wood-cement particleboard facades to enhance the impact characteristics of concrete crash barriers. CHAPTER 2 INTRODUCTION AND LITERATURE REVIEW 2.1 Introduction Wood cement particle composites have been used in the manufacturing of building materials for more than 60 years (Wolfe, 1997). As a construction material, the composite products have primarily been used as nonstructural members, and applications have mainly been based on the non-structural advantages of the composite: cost effectiveness, resistance to decay and insects, fire resistance, and thermal insulation. In the last decade, the composite has been successfully used for structural members in construction, and research on its material properties and its potential in engineering applications has increased (Kurfiel, 1995; RBAC Newsletter, 2002). The literature review presented in this chapter focuses mainly on the description of the development of the technology of wood-cement composites, and is followed by some concrete crash barriers and finite element simulation in highway crash barrier engineering. 2.2 History and Development of Wood-Cement Composites The concept of combining inorganic binders with wood or agricultural biomass can be traced back several thousands of year to ancient ancient time. Incorporating wheat or rice straw with mud to produce bricks has it roots in prehistory. Such inorganic- bonded composites are still used in many parts of the world. Mixing straw with mud improves workability, impact resistance and reduces fracture development by providing reinforcing fibers (Won, 1995). The timeline for the development of inorganic-bonded wood composites in modern times is shown in Table 2.1. The term “inorganic-bonded wood composites” generally refers to mineral-bonded wood products where the minerals mainly include magnesite, gypsum and cement. Table 2.1 Industrial Production of Inorganic-Bonded Wood Composites (Moslemi, 1988) Year Production 1900 Magnesite-bonded boards 1905 Gypsum-bonded excelsior board 1915 Magnesite-bonded excelsior board 1915 Cement-bonded excelsior board 1927 Molded wood-cement products 1937 Resin-bonded particleboards 1942 Cement-bonded wood composite panels 1965 Gypsum fiberboards (shredded paper) 1972 Magnesite-bonded wood composite panel 1982 Gypsum particleboard Wood-cement particle composites are a special type of wood-cement composites. There are three main types of wood-cement composites: (1) wood-wool cement composites (WW CC), (2) wood-fiber cement composites (WFCC) and (3) wood-cement particleboard (W CPB). The WWCC was first developed in Europe in the 19208 (Moslerni and Hamel, 1989) and it is manufacturated in many countries around the world. The WFCC were developed primarily as a substitute for asbestos-cement and have a history of about 25 to 30 years (Wolfe, 1997). Research in Europe in the 19203 led to the common practice of using wood chips in cement to make building blocks (Wolfe, 1997). This application is perhaps the origin of WCPB. However, as a product in commercial industry, WCPB was developed in the 1960s. The industry was stimulated in Europe by lumber shortages and in the United States by large quantities of waste softwood from wood manufacturing industries. The technology of making wood cement composites has many similarities to that used to manufacture resin-bonded wood particleboard (Moslerni and Hamel, 1989). 2.3 Environmental Risk of CCA-Treated Wood Chromated copper arsenate (CCA) is a water-borne preservative containing arsenic, chromium and copper. It is used for the long—term protection of wood against attack by fungi, insects and marine borers. Applying wood preservatives extends the productive life of wood and helps reduce demand for forest resources. Prior to the wood being treated, small cuts are made into the wood surface to help the penetration of the CCA preservative solution. The wood is stacked and loaded into a sealed chamber where the wood’s natural moisture is removed by vacuum. Then the chamber is pressurized, forcing the CCA solution into the wood. A vacuum is then used to extract any excess solution. The wood is removed fiom the chamber and dried (Health Canada, 2003). Waterborne preservatives today account for the vast majority of chemicals used in building applications. These waterborne chemicals are used in pressure treating only include chromated copper arsenate (CCA), ammoniacal copper zinc arsenate (ACZA), and several others. CCA accounted for 94% of the waterborne chemicals used in 1995. While the primary chemicals in CCA are highly toxic and are regulated as pesticides by the Environmental Protection Agency (EPA), they are bonded quite tightly to the wood during fixing, so leaching from the wood is minimal under normal usage conditions (EBN, 1997). There are some important benefits of treating wood with CCA, the most significant of which is increasing the life of wood for outdoor applications. Older preservatives, such as pentachlorophenal and creosote, pose considerable health risk to users of the wood, but new waterborne preservatives, such as CCA, are safer. They are safer in part because the toxins have a strong chemical bond with wood and are fixed in the wood. However, disposing of treated wood at the end of its life has become a serious problem (ENB, 1997). CCA-treated wood is used primarily for structures intended for outdoor settings and is commonly used in residential construction such as playground structures, fences, gazebos and decks. It is also used for industrial uses such as utility and construction poles, marine timbers and pilings. In 1993, an estimated 5 billion board feet, or 6.5 million tons, of wood were CCA treated and will be removed from service after approximately 27 years in 2020. This figure does not include the 72 million utility poles or 15 million ties treated annually with creosote or pentachlorophenol or other oilbome preservatives (Stalker, 1993; Mickleright, 1993). A major challenge facing the wood preservative industry today is how to deal with this massive quantity of waste wood in the coming decade. Based on a 30-year service-life, researchers at the Forest Products Laboratory (FPL) in Madison, Wisconsin estimate that 2.5 billion board feet per year (6 million m3/year) of treated-wood products (all types of preservative treatments) are currently entering the solid-waste stream, and that level will increase to 8 billion board feet per year (19 million m3/yr) by the year 2020 (EBN, 1997). The environmental hazards of CCA-treated wood are related to the high toxicity of copper, chromium and arsenic to non-target organisms in freshwater and marine environments. The potential risk depends on the exposure, i.e., the amount of CCA being leached from treated wood into the aquatic ecosystem, directly or indirectly. In general, small ground-based structures made from CCA-treated wood that are properly treated and fixed are unlikely to cause any environmental hazard. There is some data that indicates that some sealants can reduce surface dislodgeability and leachability of the preservative chemicals. This data is being considered as part of the CCA reevaluation. The environmental risk of CCA-treated wood coming into contact with freshwater and marine environments (including wetlands) is greater than in terrestrial environments and possible restrictions on aquatic use are currently being assessed. Recently, the US. Consumer Product Safety Commission (CPSC) released a risk assessment of CCA-treated wood on playground structures. This assessment concluded that children playing on playground equipment built with CCA-treated wood might have a slightly increased risk of developing cancer. However, at this time, no further action has been recommended by the CPSC (Health Canada, 2003). For the general public, on the one hand, disposal in landfills may produce environmental problems. It is increasingly difficult to dispose solid wood in landfills because it is a high volume material and deterioration is questionable when necessary requirements for biodegradation are not met. On the other hand, Stalker (1993) reported a quoted cost by landfill operators of $150 US per utility pole. The cost of disposal and the current level of environmental awareness will reduce land filling as an attractive alternative for disposal of treated wood (Cooper, 1994; Marer and Grimes, 1992). In addition, CCA-treated wood should never be burned because the heavy metals in CCA are not destroyed; the chromium and copper become concentrated in the ash, while the arsenic becomes a vapor that will escapes into air (ENB, 1997). NBC10.com (2003) reported that a single 12-foot, 2 (in.) x 6 (in.) piece of lumber contains about 27 grams of arsenic — enough to kill 250 adults. Burning CCA releases the strong chemical bond that holds the arsenic bound to the wood. As a result, the disposal of preservative-treated wood products removed from service is problematic. Therefore an attractive solution for the after service disposal of treated wood is reconstituted wood products. Recycled treated wood or urban wood, if properly managed, can be a good source of lumber or of fiber for engineered wood products such as hardboard, fiberboard, particleboard and cement-bonded particleboard. Recycling waste into wood composite products becomes increasingly attractive because it not only benefits the environment but also has economic value. 2.4 Wood and Cement 2.4.1 Wood Wood is divided into two broad classes, usually refered to as “hardwood” and “softwood”. Needle-like leaves characterize softwood trees. Such trees are known commonly as evergreens. In contrast, hardwood trees have broad leaves, which generally change color and drop in the fall in cold climatic zones. Hardwood species grow in every major region of the United States. On the worldwide basis, hardwood is dominant. They are found in most areas of the world 10 (Table 2.2). In total, hardwood growing stock has been estimated to exist in volumes almost double that of softwoods. However, North America and the former USSR softwood are dominant in total volume. Table 2.2 Area of Forestland in the World by Geographic Location and Species Group— 1980 (Haygreen, 1989) Area Total Softwoods Hardwoods (thousand ha) North America 807,092 533,075 274,017 Latin America 915,019 20,474 894,545 Europe 158,902 97,989 60,913 Afiica 743,713 13,891 729,822 Asia 468,230 102,238 365,992 USSR 928,600 679,900 248,700 Pacific area 298,947 15,995 282,952 World 4,320,503 1,463,562 2,856,941 Source: FAO (1985). Wood is composed principally of carbon, hydrogen, and oxygen. Table 2.3 shows the chemical composition of a typical North American wood and shows carbon to be the dominant element on a weight basis. Table 2.3 Elemental Composition of Wood (Haygreen, 1989) Element Percent of Dry Weight Carbon 49 Hydrogen 6 Oxygen 44 Nitrogen slight amounts Ash 0.1 The elemental constituents of wood are combined into a number of organic polymers: cellulose, hemicellulose, and ligin. Table 2.4 shows the aproximate percent of dry weight of each in hardwood and softwood. ll Table 2.4 Organic Constituents of Wood (Haygreen, 1989) Wood Type Cellulose Hemicellulose Lignin (% dry weight) Hardwood 40-44 1 5-35 18-25 Softwood 40-44 20-32 25-35 Softwoods have a uniform arrangement of a few cell types and therefore usally do not have a distinctive appearance. Hardwoods, on the other hand, are composed of widely varying proportions of markedly different kinds of cells and thus often have a unique appearance. The physical differences between hardwood and softwood are listed in Table 2.5. Figure 2.1 and Figure 2.2 show the cell types of softwood and hardwood. Table 2.5 Physical Differences Between Hardwood and Softwood (Haygreen, 1989) Hardwood Softwood Many types of cells few types of cells Contain vessels no vessels Wide rays (30% of wood volume) narrow rays ( 5-7% of wood volume) Not aligned in straight radial rows Straight radial rowsof cells 12 Figure 2.1 Softwood: Sitka sprue (x 75), (Haygreen, 198 Latewood vessels Earlywood vessels Figure 2.2 Hardwood: Red oak (x 50), (Haygreen, 1989) (Scaning electron micrograph by Josefina Gonzalez, Forintek Canada Corp. Vancouver, B.C.) l3 Currently, the wood used in wood-cement composites are generally from softwood. Figure 2.3 (Marta, 1972) shows the various sizes and shapes of wood elements included in wood composites. For wood-cement composites, the wood materials in the second and third rows in Figure 2.3 are generally used. Figure 2.3 Most common forms of wood composites elements (Marra, 1972) The wood particles are produced by a special cutting machine. A variety of machines including refiners, hammers, flakers, and waferizers can be used to produce the type of furnish (particles used to make the board) desired. These machines grind, cut, or tear the wood into a range of particle sizes. Figure 2.4 illustrate the parts of a ring flaker. This machine has knives that cut thin particles fi'om whatever kind of wood is fed to it. A general disk refiner is shown in Figure 2.5 and is used to prepare small fiberlike particles. Front view ' Flakes Impeller Knife ring Figure 2.4 Element of a knife-ring flaker (Haygreen, 1989) - , Disk Main components and plate plates of a disk refiner Revolving disk :6 Gap (adjustable) Refined particles or fiber Typical disk plates Figure 2.5 Main Component and plates of a disk refiner (Haygreen, 1989) 2.4.2 Cement An inorganic binder which has found commercial use in the field of certain wood particle panels is Portland cement. This binder is used in the manufacture of products intended for service in structural applications which may or may not be load bearing. Portland cement contains four basic chemical elements, silicon, aluminum, iron, and calcium, usually in oxidized forms (Moslemi, 1974). Portland cement is a gray powder that consists of angular particles typically in the size range of l to 50 pm. It is produced by pulverizing a clinker with calcium sulfate. The clinker is a heterogeneous mixture of several minerals produced by high-temperature reactions between calcium oxide and silica, alumina, and iron oxide. When Portland cement is dispersed in water, the calcium sulfate and the high-temperature compounds of calcium go into solution, and the liquid phase becomes rapidly saturated with various ionic species. As a result of combinations between calcium, sulfate, aluminate, and hydroxyl ions within a certain time of cement hydration, different crystals of calcium chemical compounds are created and finally solid cement paste is formed. Portland cement was formally used in manufacturing wood cement composites in 1928 (Maloney, 1977). Nowadays, in wood cement composites, Portland cement (Type I) is generally used as a binder in the wood cement composites. 2.4.3 Wood cement compatibility In wood-cement composites, the compatibility between wood and cement is a major concern. Wood species are not compatible with cement because soluble carbohydrates and certain extracts in the wood inhibit the setting and hardening of cement. In fact, in some instances, the influence of such substances is so severe that the cement binder is inhibited from setting at all regardless of the amount of time allowed. This inhibitory effect appears to be more pronounced in hardwood compared to softwoods due to the existence of the type of constituents that retard or prohibit element setting (Moslemi, 1974). To reduce the inhibitory effects of wood on cement setting, various measures have been taken. One of these consists of extracting sugars and other water soluble materials with hot water. The wood particles are soaked in hot water for a period of time. The soak duration depends on a number of factors such as the temperature of the hot water and the amount of inhibitory extractives present. The addition of various chemical l7 additives also have been found useful in reducing setting time. A major compound used in this connection is calcium chloride. Clare (1956) states that calcium chloride solutions of 1 - 3 percent are necessary to neutralize the effect of 0.1 percent sugar in the soil cement mixtures. Further increases in the level of calcium chloride, however, have been found to reduce strength in such mixtures. Miller (1987) studied the effects of carbohydates on the tensile strength and hydration characteristics of Portland cement. He concluded that sugars and other compounds in wood are detrimental to cement hydration and strength. When wood is mixed with cement, the setting time of cement increases and the cement strength decreases. However, if wood particles are treated with special chemicals, the compatibility between wood and cement may be dramatically improved. Several studies have suggested that mechanical properties of wood based composites made of CCA treated fiber or particles are lower than those of untreated firmish (Vicks, 1990; Gertjejansen et al., 1988; Suzuki, 1993). The reduction in mechanical and physical properties was attributed to the surface modification of the woody materials by preservative treatment or the interaction between the preservatives and the resin. However, for cement-bonded particleboard, Schmidt et a1. (1994) reported that CCA treated red pine particles produced strong wood-cement composites compared to untreated wood. Generally the CCA treated wood has a better compatibility with cement, while, untreated wood has a poor compatibility with cement during cement hydration. Most wood waste generated by manufacturing industries is treated with CCA. Consequently, in present-day wood-cement particleboard, the wood particles are 18 generally made fiom wood treated with CCA. Previous studies indicate that CCA-treated wood has improved compatibility with cement (Schmidt, 1994; Hsu, 1994). 2.5 Bending Strength of Wood-Cement Particleboard Most previous research on the mechanical characteristics of wood-cement composites has focused on bending strength. Through bending tests, the modulus of rupture (MOR) and modulus of elasticity (MOE) are investigated. In general, the MOR is the primary measure of the quality of wood-cement particleboard. Wolfe (1997) reported that the maximtun MOR of wood-cement particleboard is typically less than 10 MPa. 2.5.1 Elasto-degrading plastic behavior In general, wood-cement particleboard displays an elasto-degrading plastic behavior under flexural loadings due to the bridging action of wood particles (Wolfe, 1999). Figure 2.6 shows the characteristics of the load-deformation curve of wood- cement particleboard under a three-point bending test. The response is elastic until the first crack forms, then displays a reduction in stiffness until the peak load. The load carrying capability degrades after the peak load but large deformations are sustained before failure. 19 fi Load Pmax Maximum load First Crack Deformation > Figure 2.6. Typical load-deformation curve of wood-cement particleboard under bending (Wolfe, 1999) Won (1995) reported that the load-deflection curves of WCPB under bending loads show elasto-plastic behavior both for specimens cured in air and those with accelerated curing using C02. Figure 2.7 shows typical flexural stress-deflection curves. 20 10. ,3 8 _ C02 - Aspen 9.. E . V 6 _ C02 — Southern pine fl) 8 , a 4 Control '3 .- '5 5 E. 2 _ . o I I l l l 0 2 4 6 8 10 Deflection (mm) (a) Wood/cement Ratio = 0.28 (Cement/wood ratio = 3.57) 10 C02 - Aspen ,3 C02 — Southern pine o. E f a i E: Deflection (mm) (b) Wood/cement Ratio = 0.35 (Cement/wood ratio = 2.86) Figure 2.7 F lexural stress vs. deflection curves for WCPB with normal and accelerated curing (Won, 1995) 21 2.5.2 Effect of cement/wood ratio The cement/wood ratio is an important parameter in the manufacturing of wood- cement particleboard because it impacts the weight to strength ratio and the cost. At present, commercially manufactured boards are produced in the range of 2.75 to 3.0 parts of cement to 1.0 part of wood (Bison and Creten, 1977). Presternon (1976) indicated that WCPB had higher bending strength properties when the cement/wood ratio was increased from 0.75 to 1.5. Moslemi and Pfister (1987) reported that the MOR of wood-cement flakeboard increased as the cement/wood ratio was lowered from 3.0 to 1.5. In their study, the wood particles were wood flakes with a thickness of 0.56 mm and length and width fiom 12 to 25 mm. They used Portland cement types III and 1. Their test results are summarized in Figure 2.8. Lee (1985) reported that an increase of the cement/wood ratios above 2.0 had an adverse effect on bending stiffness and strength of wood excelsior board. Oyagade (1990) conducted bending tests with cement/wood ratios of 1.55, 2.33 and 3.10. This study indicated that at a constant board density, a decrease in cement/wood ratio generally improved the bending properties. 22 MOR (psi) __ TypeI- 14daycure ----—- TypeIII—l4daycure 2500 ' ‘ ................. Type I _ 28 day cure ,,.....:“ ‘ — — — - Type III — 28 day cure \“ \ \\ \‘ x \ \ x“.-.---“-"--.”--_. 2400 2300 2200 2100 1.5 2.0 2.5 3.0 Cement/wood ratio Figure 2.8. Variation of MOR with cement-wood ratio (Moslemi and Pfister, 1987) 2.5.3 Effect of manufacturing method on strength The manufacturing method for WCPB is being continually improved. Different manufacturing methods can lead to significant changes in the material properties of WCBP, such as strength and durability. The following two major of manufacturing methods are general used for WCPB: a. Thickness control and laboratory curing at 65 % relative humidity. b. Thickness control and C02 accelerated curing. Thickness control means that the specimen is manufactured to a predetermined thickness by pressing specimens in a hydraulic press. Laboratory curing is the most common curing method. In this method, specimens are cured at a temperature of 20 °C and 65% relative humidity for 28 days after they are removed from the press. 23 In the accelerated C02 curing method, after a few hours of setting under pressure, the specimens are steamed with CO2 for 5 to 8 hours for accelerated curing. This method dramatically shortens the manufacturing period. Won (1995) reported that the bending strength of wood cement particleboard cured with C02 is much higher than those cured in air. Figure 2.7 shows the differences in flexural stress between C02-cured and air-cured (control) specimens. Zhou and Kamdem (2001) reported that air curing at 20C° and 100% relative humidity for 28 days produced specimens with higher bending strength than those cured at 65 % relative humidity. 2.6 Compressive Strength of Wood-Cement Particle Composites Studies on the compressive strength of WCPB have been much fewer than those on flexural strength. With the application of wood-cement particle bricks in loading bearing walls, the compressive strength has recently received more attention. Wolfe (1997 and 1999) reported that the characteristics of the compressive load- deformation curve are similar to those for the bending test shown in Figure 2.6. In his study, the load displacement plots exhibited linear behavior up to 60 to 75% of the maximum load, at which point the rigid cement matrix began to crack. As the material began to fail, the material exhibited plastic behavior. 24 Research on hardwood-cement particle composites (Blankenhor, 1994) indicated that as the amount of red maple and hardwood pulp increased, the compressive strength decreased. Figure 2.9 shows the compressive test results. I a .9 . *5 I S 3" 5 C E a E i 8 . i 0 0.1 0.2 0.3 0.4 0.5 i Wood/Wrath Figure 2.9. Compressive strength vs. wood/cement ratio (Blankenhor, 1994) Sorfa (1984) reported that WCPB bricks developed for use as supports in mines exhibited compression properties similar to those of wood loaded perpendicular to the grain. The load-deformation curves were initially linear until matrix cracking, after which they softened (Figure 2.10). 25 600 . I. Wood : Cement 500 *- .. A 400 I' :9; I. 300 ,. '8 o I- .—I 200 L- P 100 - 0 0 Deformation (mm) Figure 2.10. Compressive load vs. deformation for WCP bricks (Sorfa, 1984) 2.7 Durability The major advantage of WCPB over resin bonded wood particleboard is that WCPB can be used for either indoor or outdoor applications, while resin bonded wood particleboard can only be used as interior material because it is sensitive to moisture and susceptible to damage by fire and insects. Won (1995) conducted flexural tests on WCPB subjected to 25 cycles of accelerated wetting-drying. He found that in general, repeated wetting-drying cycles led to increased stiffiress and reduced toughness of WCPB, and the effects on flexural strength were mixed. Figure 2.1 1 shows the wetting-drying test results. 26 Won (1995) also reported that repeated freezing-thawing cycles led to increased stiffness and reduced toughness values, and the effects on flexural strength were mixed. Figure 2.12 shows the freezing-thawing test results. Wolfe (1999) reported that freezing-thawing tests on the wood-cement particleboard support the premise that these composites can be designed to meet the durability requirements for highway sound barriers. Sirnatupang (1990) studied the durability of conventional (air curing) and rapidly curing (using C02) cement-bonded wood particleboard. He concluded that conventionally made cement-bonded wood particleboards have higher bending strength and are also more durable. However, the properties of the rapidly setting boards fulfill the requirements of existing standards. Dinwoodies (1991) and Karam (1992) demonstrated that wood-cement particleboard could be fabricated to resist cyclic moisture and temperature effects. 27 cor-ASP!!! (W0) E 8 ” cox-Aspen é (XL-SP. (VD) a 6 oo,-s. P. 8 5 4 ’ cmmp) '31 Control a ‘ i5 2 LL. 0 I I l J 0 2 4 6 8 10 Deflection (mm) Figure 2.11 Flexural strength vs. deflection under wetting and drying for wood/cement ratio of 0.28 (Won, 1995) Flexural strength (MPa) Deflection (mm) Figure 2.12 Flexural strength vs. deflection under freezing and thawing for wood/cement = 0.28 (Won, 1995) 28 2.8 Insulation Properties Wood cement composites provide very good insulation, both thermally and acoustically. The advantageous insulation properties make these composites attractive for building applications. 2.8.1 Thermal properties The thermal property of composite materials is generally related to the porosity of the composites. Composites with higher porosity usually have higher thermal resistance. Because of its relatively low density, wood-cement particleboard has good thermal properties. As reported by Eltomation Corporation (2003), the thermal resistance R-value for 2.5 cm thick wood-wool cement boards is 5. The R-value is the resistance of one square meter of the material subject to a one degree temperature difference. The equation of thermal resistance R-value can be expressed as: _ AAT W R (2.1) where R is the thermal resistance value in units of mzk/W , A is the surface area Of the heat flows in units of square meter, A T is temperature difference between the warm and cold sides of the material, and W is the resultant heat flow in units of Watt. Southern pine excelsior cement board with a thickness of 5 cm has an R-value of 4.0 (Concrete Products, 1984). Lee (1985) reported that wood excelsior cement board with a thickness of 5 cm has an R-value (thermal resistance) of 3.5. Lee (1985) concluded that the thermal conductivity or thermal resistant value is related to the density of the board and the density of the wood. For a given density of the board, lower density wood aggregate yields aboard with higher thermal resistance. 29 2.8.2 Acoustic properties Wood-cement composites are considered to have good sound absorption ability. Wolfe (1997) reported that natural fiber cement composites have good sound absorption properties, and can be used to reduce noise. Wolfe (1999) reported that the Wisconsin DOT has used WCPB for highway sound barriers. Neithalath (2003) reported an experimental test on the acoustic performance of wood fiber cement composites. The test results indicate that wood fiber cement composites have a strong potential for absorbing sound. He further concluded that the sound absorption coefficient of the wood fiber-cement composites increases with an increase of wood fiber volume due to the generation of an increased number of porous channels by wood fibers in the cement matrix. Eltomation, the world’s largest wood-cement composites supplier, reported the following sound absorption data for wood-wool cement boards (Eltomation, 2003): 0 Resistance of a plastered wall of 5 cm wood wool cement boards is 36-40 decibel. 0 Resistance of a plastered double wall with air space between WWCBs is 53-57 decibel. 0 Noise reduction coefficient for a 2.5 cm thick board is 0.7. In comparison, the acoustic resistance of a permanent shuttered wall with 12 cm concrete core is 54-56 decibel. 2.8.3 Fire resistance According to Eltomation (2003) a 5 cm thick wood-wool cement board has a 1- hour fire resistance and a 10 cm thick board has a 2-hour fire resistance. Kurfiel and 30 Moslemi (1995) reported that wood cement particleboard is in a class A fire rating. To have a class A fire rating, a material should be able to withstand severe exposure to fire. 2.9 Theoretical Studies Information concerning theoretical treatment of the behavior of cement-bonded wood composites is very limited. Linear elastic fracture mechanics, the discipline concerned with failure by crack initiation and propagation, is often used to evaluate the failure mechanism in fiber reinforced concrete material. Fiber bridging is generally accepted as the enhancing mechanism in wood-cement composites. Figure 2.13 shows a schematic representation of a cross section through a fiber-reinforced matrix. The diagram shows several possible failure modes occurring before fracture of the composites. In the high stress region near the crack tip, fibers may debond from the matrix (fiber 1). Also, sufficient stress may be transferred to a fiber (fiber 2) to ultimately fracture the fiber (fiber 4). When total debonding occurs, the debonded fiber can then be pulled out from the matrix and considerable energy is absorbed by the system in the form of fiictional energy (fiber 3). It is also possible for a fiber to be left intact as the crack propagates. This process is called bridging action. 31 Figure 2.13 Schematic representation of cracking through a fiber reinforced matrix (Coutts, 1986) Different theoretical approaches have been used to predict the strength of WCPB. Dinwoodie and Paxton (1988), Sorfa (1984) and Wolfe (1999) qualitatively related strength to density. Sarja (1988) presented the following empirical formulae for the modulus of elasticity, modulus of rupture and compressive strength of cement-bonded particleboard as a function of density: f, = 4.5(p/1000) fa: p/500 (2.2) EC: 1500(p /1000)‘ where p = density at 40% humidity in kg/m3 f, = compressive strength in MPa fc, = tensile strength in MPa E = modulus of elasticity in MPa C The composite mechanics approach has been used by several researchers (Laws, 1983; Balaguru, 1992; Bodig, 1982) in the form of ‘rule of mixtures’. The rule of mixture stated in its most general form is: 32 o". = 0'me + 0'fo (2.3) where a; is the strength of the composite, 0'", is the strength of the matrix, a; is the strength of the fibers, V". is the volume fraction of the matrix, the Vf is the volume fraction of the fibers. Similarly, for the modulus of elasticity in tension, EC, the rule of mixture is written as: EC = Em (1 - VOW," + 77E, V, (2.4) Where EC, Em and Ef are the modulus of elasticity of composite, matrix and fiber, respectively. The rule of mixtures assumes that there is no effect from Poisson’s ratio and that fibers are fully bonded to the matrix before the composite cracks, i.e. equal strain in fiber and matrix. 2.10 Applications of Wood-Cement Composites The development and use of wood-cement particle composites attest to their suitability as construction materials. Wood-cement composites have been successfully used as roofing, cladding, interior wall, exterior wall, highway sound barriers, etc. The photos in Figures 2.14 to 2.25 show applications of wood-cement composites (including particleboard, strand board and wood-wool board) in building construction. 33 Figure 2.14 Siding with WCPB in Japan (Eltomation Company) Figure 2.15 Siding with WWCB in the Phillipines (Milligan, 2004) 34 Figure 2.16a WCP Block for building walls (Hoene, 1997) Figure 2.16b Exterior and interior walls with WCP blocks (Hoene, 1997) 35 Figure 2.17 Sound barrier of wood-cement particleboard in Czech Republic (CETRIS, 2005) Figure 2.18 Wood-wool cement board for roofing and walls in Phillippines (Eltomation Company) 36 Figure 2.19 Wood strand cement board for all walls and sidings in Japan (Eltomation Company) Figure 2.20 Roof decking with wood excelsior cement composites (Moslemi, 1974) 37 Figure 2.21 Wood fiber cement board as exterior-wall cladding of the Sandoz Laboratory in Basel, Switzerland, (Deppe, 1974). 2.11 Highway Barriers 2.11.1 Introduction At a number of locations on existing highways there are physical conditions that cannot be readily modified to eliminate or minimize the hazard they present to out-of- control vehicles. These include brigde piers, abutrnents, and parapet noses; heavy, nonbreakway sign supports; and high embankment slopes. At these locations, barriers are used to reduce the hazard. The term “barriers” refers to longitudinal barriers and crash cushions. Longitudinal barriers function primarily by containing and redirecting errant vehicles. Crash cushions function primarily by decelerating errant vehicles to a stop or by redirection. 38 Longitudinal barriers, including bridge railings, are generally denoted as one of three types: (a) flexible, (b) serni-rigid and (c) rigid. Figures 2.22 to 2.24 show three types of longitudinal barriers. Figure 2.23 Semi-rigid guardrail 39 Figure 2.24 Rigid concrete barrier Flexible barriers generally consist of cable barriers, which are primarily designed to contain the crashing vehicle by deforming a large amount rather than redirecting a vehicle. These are generally used in local roads. Semi-rigid barriers are usually guardrails, which are required to contain and redirect vehicles in major highways. The guardrail is allowed to have a certain amount of deflection during vehicle impact. Rigid barriers are concrete barriers required to contain and redirect vehicles in major highways. There is no significant deflection allowed for concrete barriers during vehicle impact. 2.11.2 Barrier safety data Significant improvement in highway safety has been achieved through a multitude of actions over the past three decades, but one area where serious problems still exist is the highway roadside. Crash data indicate that highway fatalities nationwide have increased by 7% since 1992 (FHWA, 1998) and more than 40% of highway fatalities involve vehicles hitting objects on the roadside, including concrete barriers. Data from 40 the US. Department of Transportation’s Fatality Analysis Reporting System, and the Insurance Institute for Highway Safety (Roadside hazards, 2001) provide the following facts: 0 12,311 people died in roadside hazard crashes in 2000, 2% more than in 1999 and about 12% more than in 1975. o 96% of roadside hazard crash deaths in 2000 occurred in single-vehicle crashes. 0 The percent of single vehicle roadside hazard crash deaths involving rollover, in 2000 (Roadside hazards, 2001) is tabulated in Table 2.6. Table 2.6 Rate of crash death on vehicle-barrier crash Barrier Type Rate of Crash Death Bridge Rail 41% Guardrail 50% Concrete /other barrier 41% The accident data shows that a large number of deaths occur as a result of vehicles impacting concrete barriers. Therefore, enhancing the impact characteristics of concrete barriers can be benificial to the motoring public. 2.11.3 Crash performance of concrete barriers Concrete Median Barriers are widely used structures on the roadways of North America. The design of concrete median barriers has been evolving since 1950’s (Marine, M. C., 1999). As a crash safety device, concrete median barriers play an important role to contain and redirect crashing vehicle. Numerous crash test research programs on concrete median barriers have been conducted from late 1960’s through 41 early 1990’s (Marine, M. C., 1999). The concrete barrier’s shape plays an important role in vehicle-barrier crashes. In general, there are three major types of concrete barriers with different shapes (Figure 2.25): 1) New Jersey (NJ) shape concrete barriers, 2) constant slope concrete barriers, and 3) vertical concrete parapets. a. NJ Shape Barrier b. Constant slope barrier c. Vertical concrete parapet Figure 2.25 Major shapes of concrete barriers For NJ shape concrete barriers, when a vehicle’s front bumper impacts the lower sloped face and slides upwards, the vehicle is lifted and part of the kinetic energy is converted to potential energy. This potential energy is converted back into kinetic energy as the vehicle returns to the ground. Vertical concrete parapet walls do not have the energy management feature of the NJ barrier, but crash tests have demonstrated that they can perform adequately (McDevitt, 2002). All of the energy absorption in an impact with a rigid vertical wall is due to crushing of the vehicle. Bumpers usually do not slide up vertical concrete walls and lift the vehicle and all four wheels tend to stay on the ground. This minimizes the potential for vehicle rollover (McDevitt, 2002). 42 On March 22, 1990, the Texas Transportation Institute conducted a field crash test of a vehicle crashing onto a portable concrete barrier. The vehicle was a Honda Civic (820C), and the barrier was a longitudinal concrete temporary barrier. Figures 2.26 to 2.27 show the barrier’s geometry, plan view of the field test demonstration. This field test indicated that the New Jersey shape barrier successfully contained and redirected the crashing vehicle. Figure 2.26 Geometry of concrete barrier (NCHRP350 Report, 1993) 43 Figure 2.27 Demonstration of field test -plan view (NCHRP350 Report, 1993) 2.12 Concrete Material Model The response of a reinforced concrete structure, such as concrete crash barrier, is partly determined by the material response of the plain concrete of which it is composed. Therefore, analysis of structural behavior to static or dynamic loading requires prediction of the concrete response to load histories. The fundamental characteristics of concrete behavior are based on the results of experimental testing of plain concrete specimens under specific, relatively simple loading histories. Elasticity and plasticity theories provide a framework for establishing a material model that describes these fundamental characteristics. Experimental data provide additional information for validating and calibrating the material model. 44 2.12.1 Biaxial and Triaxial Behavior There is a large amount of research that has been done on the behavior of concrete under biaxial loading. The biaxial strength envelope of concrete obtained by Kupfer et a1. is quite famous. Kupfer et a1. (1969) conducted a series of tests to investigate the response of plain concrete subjected to two-dimensional loading. In the investigation, concrete plates (approximately 200 mm by 200 mm by 50 mm in dimension) were loaded to failure at prescribed ratios of 61:62 with 63 equal to zero (where 0'; is the ith principal stress). Two directional loads were applied using steel brushes to minimize stresses induced through fiiction at the specimen boundaries. The failure surfaces obtained through the testing are presented in Figure 2.28. Tasuji et a1. (1978) also conducted a series of biaxial tests on concrete. They obtained a strength envelope similar to that reported Kupfer (1969). In addition to the failure surface, they also obtained the concrete’s elastic limit surface. Both surfaces are shown in Figure 2.29. The elastic limit surface has a shape similar to but smaller than the failure surface. 45 0.2 0 '1 -0.2 ' -0.4 I 1 as I ff (PSi) l --- 2700 g ‘ ' — 4450 ‘ i I '0.8 \ —-— 8350 -l.0 I \ \ -1.2 q \‘ s~ _' -l.4 Figure 2.28 Biaxial strength envelope of concrete (Kupfer et al., 1969) As shown in Figure 2.29, the maximum strength increases under a biaxial compression state. A maximum strength increase of approximately 25% is obtained at a stress ratio of 12. = 0,5 and of 16% at an equal biaxial compression stress state 01 (£2. =10 ). Under biaxial compression-tension, the compressive strength decreases 0' almost linearly as the applied tensile stress is increased. Under biaxial tension, the strength is nearly the same as that under uniaxial tension. 46 '4 92 O I». $ f. ’ 0.2 ’ 0.4 " f Failure strength 1.2- 0.6 0.8 1.0” l - _ ~< ‘- in l l l I l 2 1.0 0.8 0.6 0.4 0.2 1. 0.0 -0.2 0'2 f.- Figure 2.29 Elastic limit and maximum strength envelopes of concrete under biaxial loading (Tasuji, 1976). Green and Swanson (1973) conducted hydrostatic compression tests on concrete. The tests indicated that concrete exhibits nonlinear behavior under hydrostatic compression, as shown in Figure 2.30. The stress-strain curve of Figure 2.30 shows a reversal in curvature on loading. Upon unloading, the slope of the curvature is almost constant and approximately equal to the slope of the initial tangent for the loading curve. 47 Compressive strength: 7000 @si) Mean normal stress. Goct (ksi) o -2 -4 -s -3 Volume change, 8v (%) Figure 2.30 Behavior of concrete under hydrostatic compression (Green and Swanson, 1973). Under triaxial loading, experiments indicate that concrete has a fairly consistent failure surface that is a function of the three principal stresses (Gerstle et al., 1978). If it is assumed that concrete is isotropic, the elastic limit (onset of stable crack propagation), the onset of unstable crack propagation, and the failure limit all can be represented as surfaces in three-dimensional principal stress space. The shape of the elastic limit surface and failure surface are shown schematically in Figure 2.31. 48 0'1 Failure surface Elastic limit surface 01:62:63 02 Figure 2.31 Schematic representation of the elastic limit and failure surface of concrete 2.12.2 Characteristics of yield surface The general characteristics of the yield surface of concrete have been determined through experiments. The experimental results are used to develop mathematical failure models. The general shape of the failure surface in the principal stress space can be best described by its cross-sectional shapes in the deviatoric planes and its meridians in the meridian planes. The cross sections of the failure surface are the intersection curves between the failure surface and a deviatoric plane which is perpendicular to the hydrostatic axis with {f = constant. The meridians of the failure surface are the intersection curves between the failure surface and a plane (the meridian plane) containing the hydrostatic axis with 0 = constant. Figure 2.32 shows a geometric representation of the stress state in the principal stress space. The straight line 0N which has equal angles with the three coordinate axes is the hydrostatic axis. Deviatoric planes 49 are the planes that are perpendicular to the hydrostatic axis. Meridian planes are the planes that contain the hydrostatic axis. 0'3 A P(O' 1,0253) 0 Hydrostatic axis N 0' 1 = 62 = 0'3 5.. e 0 ’ 0'2 61 Figure 2.32 Geometric representation of the stress state in the principal stress space. 2.12.3 Failure surface of concrete under different stress states The actual behavior and strength of concrete is complicated. This behavior depends on the geometric and material properties of the aggregate and cement paste, as well as the concrete curing condition and the nature of loading. Even though no one mathematical model can be expected to completely describe the strength properties of real concrete material, simpler models or criteria must be used in representing only those characteristics that are essential to the problem at hand. Under tensile stresses concrete fails by a cleavage type of brittle fracture. Under high hydrostatic pressure, concrete can yield and flow as a ductile material on the failure or yield surface (Chen and Saleeb, 1982). 50 Under tensile loading, concrete failure can be described by Rankine’s the maximum tensile stress criterion: alzft’ 02=ft’ 03:fr (25) where 0',- are principal stresses, and f ' is the tensile strength. 1 Under high hydrostatic pressure, shearing stress criteria, such as the Tresca and Von Mises criteria, are used to predict the ductile fiacture. Tresca l l l maxli'Z—lo'l—(yZl’Eial_02|93|01—02i]:k (2'6) Von Mises f(J.)=J2-k’=0 (2.7) where k is the failure (yield) stress in pure shear. For concrete k is determined from a simple compression test (with f; used as the yield stress). In this case, k is equal to . 1 , % fc or —‘/—3=fc for the Tresca and Von Mises criteria, respectively. J2 is the second invariant of the stress deviator tensor, and is .12 = %[(0'1 «(72)2 + ((72 —0'3)2 +(o'3 —a,)"] , p = 2J2 (2.8) In the intermediate compressive stress range, failure criteria of concrete are sensitive to the hydrostatic state of stress. The simple one-parameter models described above are not adequate for describing failure in the fracture-ductile state under this intermediate level of compressive stresses, and therefore pressure-dependent failure models must be used. The simplest and most commonly used models of this type are the 51 Mohr-Coulomb and Drucker-Prager failure criteria. These are two-parameter models whose meridians depend linearly on the hydrostatic stress component, I 1 or 15 (a) 9 0'1 Compression ‘I It Tension O\ o O / ’ a: O3 0'3 0'2 Figure 2.33 Meridian and deviatoric sections for two parameter failure models: (a) Mohr-Coulomb criterion, and (b) Drucker-Prager criterion. In the Mohr-Coulomb criteria, failure is assumed to occur when the shear stress, 1:, on any plane at a point in a concrete material reaches a value that depends linearly upon the normal stress, 0', in the same plane. Mathematically, this is expressed as |t|=c—0'tan¢ (2.9) 52 where c and (P are material constants that represent the cohesion and angle of internal friction, respectively. The Mohr-coulomb failure surface has sharp corners (Figure 2.33). These corners are not mathematically convenient because the slope discontinuity at these comers can cause many difficulties and complications in numerical solution schemes. Drucker and Prager (1952) proposed a smooth approximation to the Mohr- Coulomb surface by the following simple modification of the von Mises criterion: f(1,,J,)=a1,+JZ-k=0 (2.10) orin term offiandpas “awn/3a: +p-J5k=0 (2.11) where k and a are (positive) material constants. I, is the first principal stress invariant given by, 11 20'1“}2 +03 (2.12) There are two shortcomings of the Drucker-Prager criterion in modeling concrete material: the linear relation between I1 and E (or 5 and p), and the independence with respect to the angle of similarity 6. Experiments on concrete show that relation between I1 andJZ (or 5 and p) is nonlinear or curved, and the trace of the failure surface on deviatoric sections is not circular, but depends on the angle of similarity 0. Bresler and Pister (1958) suggested a three-pararneter failure criterion with a parabolic relation between Tao: and 032., and with circular deviatoric sections. The relation between 10c, and 03c, can be expressed in the form of 53 T 0' 0' ——°“. = -b(——°€‘)+ I—“f ’ 2-13 f. a f. c f. ) ( ’ Hsieh et a1 (1982) developed a four-parameter criterion in terms of 11, J2 and maximum principal stress 07: ,/J f(1.,12,01)=a J2, +b——.2—+9—‘.—+d—I—‘.——1=0 (2.14) f f. f. f. t C where a, b, c and d are material constants. The nonlinear meridian trace and deviatoric sections of this failure model are shown in Figure 2.34. DA A Compressive meridian V \ \ \ Tensile meridian \ \ Figure 2.34 Hsieh-Ting-Chen criterion A large number of concrete models have been published in the literature. Most of the modified models give a better agreement with relevant experimental data. However, the more accurate models generally involve many parameters that are difficult to obtain 54 experimentally. In practice, the Mohr-Coulomb and Drucker-Prager failure criteria are the most commonly used models. 2.12.4 Evolution of the yield surface of concrete under multi-dimensional loading There are few investigations that have considered the evolution of the yield surface of concrete from the initial inelastic response through complete loss of strength. The concept of the evolution of the yield surface of concrete is cited from the theory of plasticity. In plasticity theory, a change of yield surface is always described by a hardening rule. There are two common hardening rules: ‘isotropic hardening’ in which a change occurs in the size of the yield surface only (all dimensions being scaled by the same constant); and ‘kinematic hardening’ in which a change occurs in the location of the yield surface. ‘Isotropic hardening’ is the more appropriate hardening rule for concrete. Chen and Han [1988] proposed a more detailed evolution of the yield surface of concrete under a variable load history (Figure 2.35). This model proposes that at the maximum load, the yield surface may appropriately be defined by the recommendations of any of several researchers [0ttosen, 1977; Hsieh et al., 1982; Willarn and Wamke, 1975]. 55 Uniaxial compressive loading path Failure surface Loading surface \ -11 - ‘ + Figure 2.35 Evolution of concrete yield surface as proposed by Chen and Han [1988]. 2.13 Finite Element Modeling for Vehicle Crash Analysis In the last four decades, the finite element method (FEM) has become the dominant technique for analyzing physical phenomena in the field of structural, solid, and fluid mechanics. The nonlinear, explicit, three-dimensional finite element analysis code DYNA3D developed in the 19705 has made it possible to analyze contact impact problems. The first full vehicle car crash model was built and analyzed in the mid-19808 (Du Dois, 1999). Nowadays, crash simulation has become a routine task in vehicle design. However, making a high quality finite element (FE) model that can match actual vehicle behavior is still a formidable challenge for engineers. A high quality FE model should not only have good geometry with high quality elements, but also have good material modeling, contact modeling and control commands. 56 2.13.1 Brief summary of formulations LS-DYNA (Hallquist, 1999) is a nonlinear, dynamic, three-dirnensional finite element analysis code that evolved from DYNA3D. It is being widely used from the automotive to the biomechanics fields. LS-DYNA uses a Lagrangian formulation in which the mesh moves with the material. Formulation in fluid dynamics is, in contrast, Eulerian, and the FE mesh remains fixed in space. In LS-DYNA, conditions of equilibrium are derived by the principle of virtual work and are expressed by the following equation: M W 562', = F." (2.15) where My“ is the diagonal (lumped) mass matrix; 56:, is the acceleration at node k with respect to degree of fi'eedom I; F i,- is the sum of the internal and external forces; and the superscript n refers to the n-th integration time step. The diagonal mass matrix enables equation (2.14) to be solved easily for the accelerations. The velocities and displacements are then obtained through the explicit central difference method: 1 "—— l o -2- - O 2 n can x0. — xi]. + At xi}. - n+1 - n n+:li "r”; xi}. = xi]. ‘1' At xij (2.16) l n+— At 2 = %(At"+' + At") 57 where At is the integration time step. 2.13.2 Time integration The central difference method is an explicit integration method that is conditionally stable. If At is too large, the method becomes unstable. If At is much smaller than necessary, computations become expensive. Therefore, it is necessary to choose the time step At so that the method is stable and effective. The stability condition is given by the Courant, Friedrichs, and Lewy condition. At 3 5 (2.17) C where c = E / p is the speed at which information travels in the element, E is the modulus of elasticity of the material, and p is the density of the material. L is the characteristic length of elements. The physical interpretation of this condition is that At must be small enough so that information does not propagate across more than one element per time step. 2.13.3 Contact algorithm The general contact approach taken in LS-DYNA is referred to as the “penalty method.” When a node penetrates a surface, it is opposed by a linear spring force that acts normal to the surface. This force is calculated using plate theory based on the depth of the penetration and the stiffness of the surface element. If friction is specified, then the friction force is calculated from the normal force. A node trying to penetrate the surface is usually referred to as the “slave” node, and the surface it is trying to penetrate is the 58 “master segment.” These terms appeared in the finite difference literature when most contact algorithms were not symmetric. 2.13.4 Force and displacement field quantities The LS-DYNA analysis mainly outputs force field quantities and displacement field quantities. The force field quantities mainly include stresses and strains, and the displacement field quantities mainly include displacements, velocities and accelerations. In LS-DYNA analysis, force field quantities vary over the element. To reduce the CPU time, it is assumed that the stress and strain are constant over the element and equal to the values calculated at the center of the element (or at the integration point). However, the displacement field quantities (acceleration, velocity and displacement) are evaluated at the nodal points. 2.13.5 Simulation of barrier crash tests using LS-DYNA Designing safer roadside crash barriers in highway systems is a primary goal of the state DOTS and the Federal Highway Administration (FHWA). The crashworthiness of some roadside barriers has been evaluated through full-scale field-testing. Crash testing has been carried out for many years but at considerable expense. If accurate computational models can be developed and then used to predict the effects of vehicle- barrier collisions, enhanced designs of such hardware systems can be achieved more efficiently. Finite element analysis based upon the failure mechanics of traditional materials provides the best computational tool with which to undertake research that will lead to a 59 better understanding of the behavior of roadside safety structures. This will eventually lead to the formulation of improved designs, possibly utilizing new high-perforrnance materials in the fabrication of roadside safety structures. Previous simulation studies of vehicles impacting a guardrail (Plaxico, 1995) and a concrete barrier (Nilsson, 1998) show that the finite element simulations of vehicle- barrier impacts provide good agreement with the results of full-scale field tests. Figures 2.36 and Figure 2.37 Show a crash simulation using LS-DYNA computer program conducted at Texas A&M University in 1999 and a crash field test conducted by the Washington State DOT in 1998 on a new portable concrete barriers. Figure 2.36 Crash field test (front view) Figure 2.37 Crash Simulation (front view) (Roger, 2002) (Roger, 2002) Comparing Figure 2.36 with Figure 2.37, the vehicle’s frontal right corner deformation and the shape of the deformed concrete barrier are almost identical. The computer crash simulation with LS-DYNA provides an excellent prediction of the vehicles motion during impact. 60 Figures 2.38 and 2.39 show the crash simulation and crash field test on a longitudinal concrete barrier conducted by the National Crash Analysis Center in 1995 (Zaouk, 1995). Again, the simulation predicts the motion of the vehicle quite well. The simulation also provide insights that are not available from field tests about the design parameters such as detailed material responses. t =0 ms t =75 ms t =120 ms t =240 ms Figure 2.38 Crash field test Figure 2.39 Crash simulation (plan view) (plan view) 61 CHAPTER 3 IMPROVED MANUFACTURING PROCESS AND FLEXURAL PERFORMANCE 3.1 Introduction The manufacturing of cement-bonded particleboard is similar to that of resin- bonded particleboard. Making wood-cement particleboard stronger and tougher is the primary goal of the wood-cement composite industry. Better manufacturing processes have been developed to create high quality wood-cement particleboards. Up to now, two major modifications of the conventional manufacturing process for wood-cement particleboard are generally employed. One of these is the accelerated process with CO2 injection that greatly shortens the manufacturing time. Another is the addition of chemical additives to improve the bonding strength between wood particles and the cement matrix. Sirnatupang (1990) studied the performances of conventional (air curing) and rapidly cured (using C02) cement-bonded wood particleboard. He concluded that conventionally cured cement-bonded wood particleboards have higher bending strength and are also more durable. However, the properties of the rapidly cured boards fulfill the requirements of existing standards (Hsu, 1995). Chemical additives in wood cement composites does improve the bending strength of the composites, but the improvement is limited. And as with the C02 injection process, the chemical additive increases the manufacturing cost. 62 In the research reported herein, a pressure controlled and fully saturated curing process was investigated. This manufacturing process yields Significant advantages over currently used manufacturing procedures. A total of 70 flexural specimens with different cement/wood ratios were fabricated using the fully saturated curing process and tested. In addition to the effect of the curing process the effect of the cement/wood ratio on the strength of wood-cement particleboard also was investigated. 3.2 Pressure Controlled and Fully Saturated Curing Process In the pressure controlled and fully saturated curing process, the particleboard is pressed with a constant pressure and is fully saturated in water for a 28-day curing period. 3.2.1 Advantages of pressure controlled and fully saturated curing process In the currently used accelerated and air curing methods, wood particles shrink during the curing period. The shrinkage induces some degree of debonding between the wood particles and the cement matrix before the cement is fully hardened. Further, the debonding action weakens the bond strength between wood particles and the cement matrix resulting in the particleboard having a lower material strength. The fully saturated curing procedure improves bond strength between wood particles and the cement matrix. The bond strength between wood particles and cement is related to the interlock between the irregular surfaces of wood particles and the cement matrix. Because wood particles do not shrink in water during the 28-day curing period due to the fully saturated condition, the interface between wood particles and the cement 63 matrix provides considerable bond strength. Pressure controlled manufacturing with fully saturated curing should therefore produce superior wood-cement particleboard. In addition, in the pressure controlled manufacturing process specimens with different cement/wood ratios experience the same pressure during the setting period and the cement and wood particles in the specimens develop the same internal prestresses. Therefore, specimens made by this process yield stronger correlations between material properties and cement/wood ratios. 3.2.2 Materials The materials used in this research are soft wood (southern yellow pine) particles, Portland cement (Type I) and water. The particles were made from waste wood treated with chromated copper arsenate (CCA). In this study, CCA-treated wood (southern yellow pine) removed from service is used to produce wood particles. Figure 3.1 shows a typical cross section of CCA-treated southern yellow pine removed from service. The wood particles were produced through two steps. First, crushed wood is placed into a cutting machine (Figure 3.3) to produce raw wood particles. Second, the particles are separated by size by sieving with Tyler Screens (Figure 3.4). Particles (Figure 3.2) with size fiom 2 to 8 mm long x 1.0 mm in diameter are selected for making the particleboard. All the wood particles used in this research were made at the Wood Technology Laboratory in the Department of Forestry at Michigan State University. 64 A ‘.~ .‘n “Figure 3.1. CCA-treated wood Figure 3.2. Wood particles I Figure 3.3. Wood particle outing machine Figure 3.4. Wood particle screener 65 3.2.3 Particleboard manufacturing All wood-cement composite Specimens were fabricated in the Concrete Material Laboratory in the Department of Civil and Environmental Engineering at Michigan State University. In making test specimens, the quantity of wood particles, water and cement required to produce particleboard measuring 315 mm (wide) by 315 mm (long) by 12~20 mm (thickness) were estimated for a given cement/wood ratio. The required quantity of wood particles, cement and water were mechanically mixed until homogenous slurry was formed. The composite slurry was transferred onto a metal mat of315 mm x 315 mm x 14 mm, and loaded onto a hydraulic press for pressing. The mat remained under pressure for 24 hours. After 24 hours of cold pressing, the particleboard was removed and put into a water container for 28 days of curing under the laboratory room environment. After 28 days of curing, the particleboard was removed from the water and left to dry in the laboratory environment for two days. A table saw was then used to out each particleboard into the test specimens with dimensions of 230 mm (long) by 100 mm (wide) by 10 to 22 mm (thick). Figures 3.5 to 3.8 show the mixer, hydraulic press, curing container and saw used to cut the board, respectively. Figure 3.9 shows the flowchart of the manufacturing process for the wood-cement particleboard. 66 Figure 3.5. Cement wood particle mixer Figure 3.6. Hydraulic press Figure 3.7. Curing in water Figure 3.8. Saw used to cut board 67 Flowchart of Wood-Cement Particleboard Manufacturing Process CCA-treated Wood I Cutting/Screenin Cement I I Wood Particles flu Dry mixing ~————> Mixing Cutting/Sizing Water I I Forming I Pressing I Setting/Hardening Under Press I Demolding I Curing I I Storage Drying/Conditioning Figure 3.9 Flowchart of manufacturing process 68 3.3 Flexural Properties of Wood-Cement Particleboard Wood-cement particleboard is presently used mainly as non-structural members in building construction. They are often subjected bending load (e. g. particleboard siding subjected to wind load). The bending strength of the wood-cement particleboard is generally used to evaluate the quality of the boards in the wood-cement composites industry and is an important property. 3.3.1 Experimental Design Wood—cement particleboard using CCA-treated softwood particles, Portland cement (Type I), and water, were fabricated as described in Section 3.1.3. The test matrix for the bending test is given in Table 3.1. All specimens had a length of 230 mm, a width of 100 mm and a thickness that varied fiom 12 to 20 m. Table 3.1 Test Matrix for Bending Test Cement/wood ratio 4.0 3.5 3.0 2.0 1.5 1.25 1.0 Number of specimens 10 10 10 10 10 10 10 3.3.2 Description of Test Bending tests were conducted to determine material properties of the wood- cernent particleboard. The American National Standards Institute Specifications for particleboard (ANSI A208.1-1993) and The American Society for Testing and Materials (standard method of evaluating the properties of wood based fiber and particle panel materials, ASTM D 1037-78, 1996) were used. 69 Three point bending tests were conducted on an INSTRON machine (Figure 3.10) to determine the modulus of rupture (MOR), modulus of elasticity (MOE) and the strain at peak load. The tests were conducted in the Department of Forestry at Michigan State University. Figure 3.11 shows the test set-up. The sizes of the test specimens is shown in Figure 3.12. Figure 3.10. INSTRON Machine Figure 3.11. Bending test set-up I— 8 g. (Thickness = 10 ~ 22 mm) a "‘ o. :2 :2 __\L_ I] 200 mm |\ ’I L 230 mm Figure 3.12 Specimen’s size 70 The loading speed was based on ASTM D 1037-78 (1996). The loading rate of the moveable crosshead of the test machine calculated as follows: N = zL2/6d (3.1) where: N = rate of motion of moving head, in./min (mm/min), z = unit rate of fiber strain, in./in.(mm/mm) of outer fiber length per minute (0.005), L = span, in. (mm) and d = depth (thickness) of specimen, in. (mm). The Specimens to be tested in the soaked condition were submerged in water at a temperature of 20° 3: 3° C for 24 hours before the test and were tested immediately upon removal from the water. 3.3.3 Test results and analysis The typical failure characteristics of the specimens under bending are shown in Figures 3.13 and 3.14. Observation of the bending test showed that failure does not generally occurs due to a straight crack but due to a network of independent cracks as shown in Figure 3.13 that are most likely caused by the wood particle’s bridging action. The cross sectional view of the particleboard’s failure (Figure 3.14) further indicates that the wood particles play a bridging action role in resisting bending load. Figure 3.13 and 3.14 Show that the wood-cement particleboard failure under bending occurs after the wood particles pull out fi'om the cement matrix. As the wood 71 particles were pulled out, the bridging action disappears and the board loses its bending capacity. Figure 3.14. Cross-section view of failure The typical load-deflection curves (Figure 3.15) show that the WCPB behaves as an elastic-degrading plastic material with significant loss of strength following the achievement of peak load. 72 140 I 120 ‘ Cement/wood = 1.5 100 . 80 i 60 2 (1b.) Cement/wood = 1.0 Load 40 i / 20 « Cement/wood = 3.0 0 - i . 0 0.02 0.04 0.06 0.08 0.1 0.12 0.14 I I I Deflection (in.) Figure 3.15. Load-deflection curves for varying cement/wood ratios The test was conducted based on the American National Standard ASTM D 1037- 78, (1996). For the static bending test, the ASTM D 103 7-78 defines the modulus of rupture and the modulus of elasticity as follows: MOR =3PL/2bd2 (3.2) MOE = PIL3/4bd3y. (3.3) where: b = width of specimen, in. (mm), d = thickness (depth) of specimen, in. (mm), L = length of span, in. (mm), 73 P = maximum load, lbf (N), P1 = load at proportional limit, lbf (N), MOR = modulus of rupture, psi (kPa), MOE = stiffness ( aparent modulus of elasticity), psi (kPa), y] = center deflection at proportional limit load, in. (mm). The measured flextural strength (modulus of rupture), modulus of elasticity and density of the wood-cement particleboard are presented in Table 3.2 and Figure 3.16 to Figure 3.18. 74 Table 3.2 Flexural Perforrnence of Wood -Cement Particleboard Manufactured with Seven Different Cement/Wood Ratios Modulus of Rupture Modulus of Elasticity Density Test Results (MPa) (MPa) (kg/m3) Mean St. Dev. Mean St. Dev. Mean St. Dev. 1.0 10.1 1 0.72 1670 180 967 52 1.25 10.33 0.63 1980 186 978 49 .2 $3 1.5 11.71 0.44 3027 305 1044 31 '8 ‘3’ E 2.0 9.53 0.68 3319 402 1151 34 O 3.0 7.03 0.29 3606 414 1329 46 3.5 7.4 0.65 4376 565 1468 67 4.0 7.31 0.71 5026 637 1551 71 Figure 3.16 indicates that a cement/wood ratio of 1.5 yields the highest modulus of rupture and the largest strain at peak load. When the cement/wood ratio is large, there are insufficient wood particles to provide effective bridging action and hence the MOR is low. When the cement/wood ratio is too low, there is insufficient binder to fully bond the fibers with the matrix. A cement/wood ratio of 1.5 appears to be optimal. Figure 3.17 shows that the modulus of elasticity increases almost linearly with increasing cement/wood ratio. Figure 3.18 shows that the density of the board increases linearly 75 with increasing cement/wood ratio. The cement/wood ratios of 1.5 and 1.0 were used for all other tests. (MPa) 5 Modulus of rupture O I I fir I I 0 l 2 3 4 5 Cement/wood ratio 6000 5000 7 4000 - 3000 - 2000 ‘ 1000 . Modulus of elasticity (MPa) O T T r I 0 1 2 3 4 5 Cement/wood ratio Figure 3.17. Correlation between MOE and cement/wood ratio 76 2000 ”a 15004 to é g 1000- E 8 500 4 0 I I I I 0 1 2 3 4 5 Cement/wood ratio Figure 3.18. Correlation between density and cement/wood ratio Toughness is generally used as a measure of energy dissipation for a material. The most common method to measure toughness is to use the load-deflection curve of a simply supported beam under bending. There are at least three procedures that are suggested to quantify toughness using the load-deflection curve obtained in static loading. As reported by ACI Committee 544 on Fiber Reinforced Concrete, the ideal way to define the toughness index I, is by the following ratio: Area under the load —deflection curve until the load reaches zero for fiber composite = 3.4 ' Area under the load —deflection curve until the ( ) load reaches zero for plain matrix 77 In equation (3.4), the energy absorbed by a fiber-reinforced composite beam is normalized by dividing it by the energy absorbed by an identical beam made with the plain matrix. While equation (3 .4) is conceptually sound, it poses a number of practical difficulties (e.g., plain concrete often suddenly collapses). In practice, the ASTM C1018 procedure is more suitable for the toughness index 1,. In the ASTM C1018 procedure, the denominator in equation (3.4) is taken as the area under the load-deflection curve up to the first crack. The first crack is assumed to occur at the point where the load-deflection curve deviates from the initial linear portion. The numerator is taken as the area under the load-deflection curve up to a certain specified deflection. Three levels of deflection, namely, 35, 5.58 and 10.55, are suggested for the numerator, where 5 is the deflection at first crack. The three suggested indices, called 15, 1,0, and 120 are defined as: I __ Area under the load - deflection curve up to 3d 3.5 5 Area under the load —deflection up to d ( ) Area It to 5.55 1l0 = p (3.6) Area up to 5 Area u to 10.56 120 = p (3.7) Area up to 5 78 7 Load Pmax Maximum load I ------- First Crack Deformation b OO 36 5.56 Figure 3.19 Toughness calculation curve (load-deformation curve) The procedure is shown schematically in Figure 3.19. If a plain concrete beam is tested under load control, the beam would break into two pieces right after the first crack occurs, yielding a toughness index of 1.0. In this research, the ASTM C1018 procedure was applied to calculate the toughness of wood-cement particle composites. Table 3.3 shows the calculated toughness index 15 for wood cement particleboard with seven different cement/wood ratios under three-point bending tests. The calculated toughness indices (15) are roughly around 6.0. 79 Table 3.3 Flexural Tougmess of Wood Cement Particleboard Cement/Wood Ratio Toughness Results 1.0 1.25 1.5 2.0 3.0 3.5 4.0 Toughness Mean 5.95 6.04 6.22 6.18 6.33 5.81 5.72 15 St. Dev. 0.11 0.08 0.16 0.21 0.25 0.22 0.33 Statistical analysis of the test results confirmed that the fully saturated curing process yielded improved flexural performance at the 95 % level of confidence. The confidence interval level is calculated by the formula: 7 + 196(3) (3.8) n where, Y is the mean value, 0’ is the standard deviation and n is the number of samples. The modulus of rupture, modulus of elasticity, density and toughness index of wood-cement particleboards with seven different cement/wood ratios are shown in Figure 3.20, Figure 3.21, Figure 3.23 and Figure 3.25, respectively. The 95% confidence interval is shown using error bars. Figure 3.22 and Figure 3.24 Show the linear regression lines for modulus of elasticity (MOE) vs. cement/wood ratio and density vs. cement/woOd ratio, respectively. The linear regression equations has the following form: (3.9) y = a + bx, with an estimate of R2 where x is the explanatory variable, y is the dependent variable, and a and b are constant. 80 The a, b and R2 are calculated from the equations: I In =20, -;)2 = in. —§)(y. 4;) lyy =Z(yi -;)2 l < b=ll In _ I”. = ——-'—x y 1 LI: 1 1‘. R2 =—1,1— ’0 n ”( ll ) t xxyy where n is the number of samples. Modulus of Rupture, (MPa) I III (3.10) Cement/wood ratio Figure 3.20 confidence interval 81 Variation of modulus of rupture vs. 10 ll 12 13 cement/wood ratio and 95% Modulus of Elasticity, (MPa) 5000 I 4000 I 3000 i 2000 1000 - (1m 1 l 1 l I 30 3.5 4.0 1.0 1.25 1.5 2.0 2.5 Cement/wood ratio Figure 3.21 Variation of modulus of elasticity vs. cement/wood ratio and 95% confidence interval 6000 y = 1015+978x 5000 R2: 102865 T— _' '1 (MPa) I .5 4000 'r .3 3000 L ‘2 l 2 2000 I A A A Testdata g 1000 I — Regression line 2 0 I I I I 0 1 2 3 4 5 Cement/wood ratio Figure 3.22 Modulus of elasticity vs. cement/wood ratio 82 Density, (kg/m3) Figure 3.23 Density, (kg/m3) 1800 1600 1400 1200 1000 800 600 400 200 1800 1600 1400 I 1200 1000 800 b 600 F- 400 _ 200 t 0.00 I 25 30 3.5 4.0 .1 1.0 1.25 1.5 2.0 Cement/wood ratio Variation of density vs. cement/wood ratio and 95% confidence interval I" y = 744 + 201x E R2 = 218 I I A Test data [ — Regression line I I I I I I 0 1 2 3 4 5 Cement/wood ratio Figure 3.24 Density vs. cement/wood ratio 83 Toughness Index, [5 .0 3 0 3.5 4.0 1.0 1.25 1.5 2 Cement/wood ratio Figure 3.25 Variation of toughness index vs. cement/wood ratio and 95% confidence interval 3.4 Discussion Flexural test results show that the pressure controlled and fully saturated curing process improves the bending strength of the wood-cement particleboard to 11.7 MPa which is higher than the commonly accepted limit of 10 MPa (Wolfe, 1996). A more reliable relationship between bending strength and cement/wood ratio was found for wood-cement particleboards manufactured using the pressure controlled and fully saturated curing process. The test results show that wood-cement particleboard with a cement/wood ratio of 1.5 yields the maximum bending strength (or modulus of rupture). Consequently, the cement/wood ratio of 1.5 was considered as an optimum value for making wood-cement particleboard. The test results also indicate that the bending strength of the composite increases with the increase of cement/wood ratio from 1.0 to 1.5 and then decreases as the cement/wood ratio increases further from 1.5 to 4.0. The correlation between bending strength and the cement/wood ratio is consistent with test 84 results reported by Prestemon (1976) that wood-cement particleboard had higher bending strength properties when the cement/wood ratio was increased from 0.75 to 1.5, and also with the results reported by Moslemi and Pfister (1987) that the modulus of rupture of wood-cement flakeboard increased as the cement/wood ratio was lowered fi'om 3.0 to 1.5. The test results also show that the modulus of elasticity increases almost linearly as the cement/wood ratio is increased from 1.0 to 4.0. And the density of the wood cement particleboard increases linearly with the increase of cement/wood ratios. The toughness indices derived from test results under bending test are around 6.0. And the results indicate that a cement/wood ratio has no significant influence on the toughness index of the particleboard. The toughness index (15) of 6.0 indicates the wood cement particleboard has a higher energy dissipation capacity comparing with steel fiber reinforced concrete that has a toughness index of 5.0. Therefore, the wood—cement particleboard can be used where the energy dissipation property is desired. 85 CHAPTER 4 COMPRESSIVE BEHAVIOR OF WOOD-CEMENT PARTICLEBOARD 4.1 Introduction Wood—cement particle composites used as structural members in building construction must often carry compressive loads. It is therefore necessary to characterize the properties of the composites under compression. The flexural properties of the wood- cement composites have been investigated extensively. Very little information is available on the compressive properties of cement bonded wood particle composites. The use of wood-cement particle bricks in load bearing walls requires information on compressive load-deformation and toughness. In most case, wood-cement composites were assumed to be isotropic, and the influence of particle orientation on mechanical properties has not been well characterized. In this research, the compressive properties of the wood-cement particleboard in directions parallel and perpendicular to the wood fiber including the failure modes, stress-strain relations, and energy dissipation are investigated. A total of 22 specimens were manufactured using Portland cement (type I) and wood particles from CCA-treated southern yellow pine. The specimens were fabricated into rectangular short columns with different aspect ratios (width/height). The cement/wood ratios by weight of the specimens were 1.5 and 1.0. 86 4.2 Experimental Design Wood-cement particleboard specimens with the aspect ratios shown in Table 4.1 were cut from thick particleboards (35 mm thick board with cement/wood ratio of 1.5 and 30 mm thick board with cement/wood ratio of 1.0). A schematic of the short column specimens is shown in Figure 4.1 and Figure 4.2 shows the loading directions. Table 4.1 shows the test matrix. Table 4.1 Test Matrix for Determination Aspect specimens Figure 4.1 Short column specimens 87 Loading perpendicular to fiber direction Loading parallel to fiber direction Figure 4.2 Loading directions 4.3 Compression Test 4.3.1 Test method The compression tests were conducted at the Wood Technology Laboratory in the Department of Forestry at Michigan State University using an INSTRON machine (Figure 4.3). A photograph of typical specimens are shown in Figure.4.4. The specimens were tested with load parallel and perpendicular to the board thickness. The procedures in ASTM D1037-78 (1996) were applied to evaluate the material properties of the laboratory manufactured particle composites. The compressive loading rate was is 0.06 inch/minute. 88 Figure 4.3 Compression test set-up on IN STRON test machine ‘- . ImIvumfl rm 9%. r Figure 4.3 Compression specimens 89 4.3.2 Failure modes Figure 4.5 shows the failure modes of specimens with an aspect ratio of 2.0 and a cement/wood ratio of 1.5 loaded parallel and perpendicular to the fiber directions. Figure 4.6 shows the failure modes for parallel and perpendicular loading on specimens with an aspect ratio of 2.0 and a cement/wood ratio of 1.0. Figure 4.7 shows the failure characteristics for parallel and perpendicular loading on specimens with an aspect ratio of 3.0 and a cement/wood ratio of 1.5. 90 a. Parallel loading b. Perpendicular loading Figure 4.5 Failure modes (h/d =2.0, cement/wood ratio = 1.5) a. Parallel loading b. Perpendicular loading Figure 4.6 Failure modes (h/d =2.0, cement/wood ratio = 1.0) a. Parallel loading b. Perpendicular loading Figure 4.7 Failure modes (h/d =3.0, cement/wood ratio = 1.5) The failure modes on all samples were independent of the cement to wood ratios and column aspect ratios used in this study. The compressive failure typically occurred along diagonal bands similar to compression-shear failure on concrete specimens. It may be concluded that short column specimens failed predominantly in shear under compressive loading irrespective of the orientation of the wood particles. 4.3.3 Compressive strength and stiffness The typical load deformation curves corresponding to the specimens shown in Figures 4.5, 4.6 and 4.7 are shown in Figures 4.8, 4.9 and 4.10, respectively. MID Parallel -800 ~ Perpendicular ,3 -600- E «1004 Dimension: 17.5 x 17.5 x 35 mm -2m . o - T T T T 0 -0.05 -0.1 -0.15 -0.2 -025 Deformation (in.) Figure 4.8 Load-deformation curve (h/d = 2.0, cement/wood = 1.5) 94 Load (lb) Load (1b.) -1m -I Parallel Perpendicular Dimension: 15 x 15 x 30 mm OJ r 02 03 04 05 05 Deformation (in.) Figure 4.9 Load deformation curves (h/d = 2.0, cement/wood =1.0) Parallel / Perpendicular Dimension: 11.7 x11.7 x 35 mm -0.05 I I T -0.1 -0.15 -0.2 -0.25 Deformation (in.) Figure 4.10 Load deformation curves (h/d = 3.0, cement/wood =1.5) 95 The load-deformation curves obtained in the tests display significant nonlinearity, and indicate that the wood-cement particleboard has the capability to absorb energy. Further, the mechanical properties are not isotropic and indicate directional dependencies. The directional properties are due to the alignment of wood particles caused by pressing during the manufacturing process. Three significant observations are made: (1) Under compression WCPB is much stiffer in the direction parallel to the particle fiber than in the perpendicular direction; (2) The deformation of the specimens in the direction perpendicular to particle orientation is much larger than in the parallel direction; (3) For an h/d ratio of 2.0, the compressive strength of specimens with cement to wood ratio of 1.5 was higher than that of specimens with a cement/wood ratio of 1.0 for both loading directions. The compressive properties of WCPB and normal concrete are shown in Table 4.2. The compressive strength of WCPC was comparable to that of normal concrete, but the strains at maximum stress and at failure were much larger than that of normal concrete. The values in Table 4.2 indicate that the highest strength for WCPB occurred when the cement/wood ratio was 1.5, the specimen aspect ratio (h/d) was 2.0, and the loading direction was parallel to the fiber direction. For this case the compressive strength of WCPB is comparable to that of normal concrete and the strain at peak stress is ten times larger than that for concrete. 96 Table 4.2 Compressive Strength and Strain at Peak Stress for WCPB and Normal Concrete Loading Mean Std. Dev Material h/d C/W Direction Strength Strain Strength Strain // 2600 0.023 243 0.002 WCPB 2-0 1-5 _L 2511 0.123 221 0.019 // 713 0.041 67 0.005 WCPB 2.0 1.0 _1_ 1808 0.284 192 0.032 // 1650 0.013 154 0.002 WCPB 3 .0 1.5 I 2060 0.094 189 0.013 Concrete _ _ _ 3000 0.002 __ _ Note: h/d=aspect ratio; C/W=cement/wood ratio; // = parallel to wood fiber direction; J. =Perpendicular to wood fiber direction; Strength=compressive strength; Strain=strain at peak stress; Concrete=normal concrete. The compressive strength for specimens loaded perpendicular to the fiber direction was smaller than that for specimens loaded parallel to the fiber direction in some cases and larger for other cases. The strain at peak stress was much larger when specimens were loaded perpendicular to the fiber direction than when they were loaded parallel to the fiber direction and 45 to 140 times larger than for normal concrete. The difference in properties for columns with aspect ratios of 2.0 and 3.0 may be attributed to the likelihood of eccentric loading for the longer specimens. The ability of WCPB to sustain large plastic deformations compared to normal concrete implies that it has a strong potential to dissipate energy. 97 Table 4.3 shows the mean and standard deviation of the stiffness of the wood- cement particleboard under compression load. The stiffnesses of the WCPB are three to four times higher when loaded parallel to the fiber direction than when loaded perpendicular to the fiber direction. Both stiffnesses are three to four times larger for a cement/wood ratio of 1.5 compared to those for a cement/wood ratio of 1.0. Table 4.3 Stiffness of Wood-Cement Particleboard Material h/d C/W Loading Mean St. Dev Direction // 1 1 78 96 WCPB 2.0 1.5 _L 400 23 // 402 34 WCPB 2.0 1.0 .1. 1 10 l 3 Notes: // = parallel to wood fiber direction; .L = perpendicular to wood fiber direction, h/d=aspect ratio; C/W=cement wood ratio 4.3.4 Toughness Toughness is a measure of the energy absorbed per unit area of material and is usually defined as the area under the load-deformation curve. ASTM C1018 is often used to calculate toughness indices. ASTM C1018 defines a set of toughness indices for fiber reinforced concrete, which are defined as the area under the load-deformation curve up to the deformations of 3, 5.5 and 10.5 times the deformation at first crack divided by the area under load-deformation curve up to the first crack. In the concrete industry, the toughness index of plain concrete is 1.0 and the toughness index of steel fiber reinforced concrete is about 5.0. 98 In this study the ASTM C1018 toughness index (15) is used to define the compressive toughness of wood-cement particleboard. The toughness index (15) is defined by the following equation: _ Area under the load — deformatio n carve up to 36 15 (4.1) Area under the load - deformatio n up to (5 where, 5 is the axial deformation up to the first crack. Table 4.4 shows the calculated toughness index 15 for WCPB with two cement/wood ratios under uniaxial compression. The calculated toughness index (15) of the WCPB is about 7.0. The toughness index 15 is close to a constant irrespective of the loading direction because the defined 36 area under the load-deformation curve can not cover the values of peak stress and strain at peak stress due to peak stress being too large. Table 4.4 Compressive Toughness of Wood-Cement Particleboard Toughness 15 Material C/W Mean St. Dev WCPB 1.5 6.99 0.41 WCPB 1.0 7.03 0.37 Figure 4.11 appears to indicate that the energy dissipation ability of the WCPB perpendicular to the fiber direction is higher than that in the direction parallel to the fiber 99 direction. However, the toughness index 15 was close to 7.0 irrespective of the loading direction. Stress (psi) I I I I 0115 0.1 015 02 025 03 «0. Strain 25 -0.4 -0.45 (1) Parallel, C/w =l.5, h/d = 2.0; (2) Perpendicular, C/w =1.5, h/d = 2.0. (3) Parallel, C/w =l.5, h/d = 3.0. (4) Perpendicular, C/w =l.5, h/d = 3.0. (5) Parallel, C/w =l.0, h/d = 2.0. (6) Perpendicular, C/w =1.0, h/d = 2.0. Figure 4.11 Stress-strain relationships of the wood-cement particleboard At the 95% level of confidence, the compressive strength, stiffness and toughness index of wood-cement particleboards with two different cement/wood ratios are shown in Figures 4.12 to 4.16. 100 A N 0.. 2 3000 V I g 2500 i 8 2000 I 5 I o 1500 > I '63 1000 .8. I g, 500 r 8 0 U 1 .5 1 .0 Cement/wood ratio Figure 4.12 Compressive strength vs. cement/wood ratio (loading parallel to fiber) E 3000 2 I v I r I "a 2500 I g I m 2000 I o | .2. I m 1500 13. . 2‘ I o 1000 U 1.0 Cement/wood ratio Figure 4.13 Compressive strength vs. cement/wood ratio (loading perpendicular to fiber) 101 1400 1200 1000 800 600 400 200 ,~'-'. 1 A; . I . ? I. 3;; 12' r -. ,_ rs' ‘, 5. ,":~ yr, '1‘ ‘TI I— Compressive stiffness, (MPa) 1 .5 l .0 Cement/wood ratio Figure 4.14 Compressive stiffness vs. cement/wood ratio (loading parallel to fiber) Compressive stiffness, (MPa) 8 O 1 .5 1.0 Cement/wood ratio Figure 4.15 Compressive stiffness vs. cement/wood ratio (loading perpendicular to fiber) 102 7.5 Compressive toughness index 15 Cement/wood ratio Figure 4.16 Compressive toughness index [S vs. cement/wood ratio (irrespective of loading direction) 4.4 Summary Compressive tests conducted on WCPB show signifficant inelastic behavior. the composite specimen fails in shear under compressive loading parallel to or perpendicular to the wood fiber direction. Composites with a cement/wood ratio of 1.5 exhibited a compressive strength comparable to that of normal concrete, but the strain at peak load was ten to forty five times larger than the strain at peak load for normal concrete depending on the direction of the compressive loading. The ability of the composites to sustain such large plastic deformations suggests that WCPB has a strong potential to dissipate energy. The toughness index I 5 for the composites with either a cement/wood ratio of 1.5 or 1.0 was about 7.0, which is seven times larger than that of normal concrete. 103 This study suggests that CCA-treated wood removed fiom service can be used for manufacturing wood-cement particleboard for use in applications where compressive strength and energy dissipation are desirable properties. 104 CHAPTER 5 IMPACT TESTS ON WOOD-CEMENT PARTICLEBOARD 5.1 Introduction Information about the impact response and energy dissipation of wood cement particle composites is needed if these composites are employed as structural members that may sustain impact loads. While the energy dissipation of wood-cement particle composites have been evaluated by measuring flexural and compressive toughness (Wolfe, 1996 and Hsu, 1995), no work appears to have been done using direct impact tests. In this study, a falling ball impact test on wood-cement particleboard was conducted to investigate the impact response and energy dissipation behavior of the composite. In order to compare its response with those of more traditional building materials, such as wood and concrete, impact tests on concrete and on a wood board resting on concrete were also conducted. These impact tests were evaluated by measuring the acceleration of a steel ball during impact. A hi gh-precision accelerometer was employed in the impact test to record the acceleration of the steel ball when it impacted different materials. A total of fifteen tests were conducted in this research for a steel ball impacting on the following surfaces: (1) wood-cement particleboard resting on concrete block, (2) wood board resting on concrete block, and (3) concrete block. In addition to the direct falling ball impact tests, multi-stress tests on wood- cement composite tubes were conducted as well. One of the purposes of this test was to 105 investigate the material behavior of the wood-cement particleboard under a multi-stress state. Another was to investigate the effect of assuming the WCPB as an elasto-plastic isotropic material by comparing test results with the results of finite element simulation that use the isotropic material model presented in Chapter 6. The compressive tests were conducted using an MTS compression machine. 5.2 Falling Ball Impact Test 5.2.1 Impact test design The falling ball impact test was designed to investigate the impact characteristics of WCPB. An accelerometer was mounted in the steel ball for recording the impact response of the ball as it impacted different materials. Three different materials were used: WCPB resting on a concrete block, wood board (wood grain parallel to horizontal plan) resting on a concrete block, and a plain concrete block. The wood cement particleboard had a dimension of 120 x 120 x 35 mm (length x width x thickness) and a cement/wood ratio of 1.5. The wood board had a dimension of 120 x 120 x 35 mm and was made of CCA-treated southern yellow pine (the same kind of wood spices for the wood particles in the wood-cement particleboard). The concrete had a dimension of 150 x 150 x 150 mm and was made of normal concrete with a compressive strength of f c = 4000 psi. The steel ball was released from rest at a height, H, of 152 mm (or 6 inches) above the impact surface. Figure 5.1 shows schematics of the impact tests. The test matrix detailing the ntunber of specimens and specimen dimensions are given in Table 5.1. 106 Concrete / a. Impact on concrete Figure 5.1 Steel ball . Wood '1 Concrete Table 5.1 Test Matrix for lrnpact Test Schematics of impact test Steel ball I b. Impact on wood on concrete c. Impact on WCPB on concrete Concrete Wood on concrete WCPB on Concrete Numbers of Test Specimens 5 5 5 Dimensions, mm 150 x 150 x 150 (concrete) 120 x 120 x 35 (wood) 120 x 120 x 35 (WCPB) In order to conduct the impact test, a test device was designed and manufactured. 5.2.2 Design of impact device 1 ball. Figure 5.2 is the release mechanism for the impact test. 07 The impact test device includes two parts: one is an impact steel ball mounted with an accelerometer, and the other is an electro-magnetic release mechanism that released the Figure 5.2 Release mechanism The impact ball selected was a solid steel ball with a diameter of 107 mm and a weight of 5.0 kg. In order to record the acceleration of the steel ball during the impact, an accelerometer was mounted in the steel ball. A schematic of the steel ball with the mounted accelerometer is shown in Figure 5.3. The accelerometer was recessed into the steel ball to protect it fi'om damage during impact. Figure 5.4 shows photographs of the ball and mount. 108 Mount bed Accelerometer d=107mm W=5kg Figure 5.3 Schematic of the impact ball Mount Impact ball with threaded hole Impact ball with mount Figure 5.4 Photographs of impact ball assembly 109 5.2.3 Impact data recording devices The impact data was recorded using an accelerometer and oscilloscope. A model 353812 piezoelectric accelerometer made by PCB Piezotronics, Inc was used. The accelerometer can measure the shock exposure experienced by space vehicles and cargo during stage separation. It may also be used to determine maximum impact acceleration levels experienced by vehicles and crash dummies. The accelerometer is a high frequency, quartz shear ICP accelerometer with a measurement range of i IOOOg (: 4905 m/sz). In addition, the accelerometer’s size (Hex x height) is 7.1 x 14.7 (mm) and its weight is 1.5 gm (0.05 oz). Figure 5.5 shows a photo of the accelerometer. I,“ I» -y - l3. Figure 5.5 353312 accelerometer Figure 5.6 Oscilloscope The oscilloscope used was an Agilent 54620A instrument made by Agilent Technologies and is shown in Figure 5.6. It is used to display the time history of the acceleration and record the test data. The oscilloscope had the capability of storing recorded data on a computer floppy disk. 110 5.2.4 Impact test set up and results The impact test on wood-cement particleboard resting on a concrete block was conducted for the purpose of determining the impact characteristics of the composite. Figure 5.7 shows the set-up for the impact test. Release mechanism Figure 5.7 Impact test setup Figure 5.8 shows the permanent deformation in the particleboard subsequent to impact by the steel ball. As shown in Figure 5.8, the impact caused an indentation of about 1.5 mm at the center of the impact area. Because the board’s deformation is permanent, a plastic deformation occurs in the wood-cement particleboard due to the 111 impact of falling steel ball. The impact did not produce a crack at the bottom of the board. Board top surface Impacted dent Figure 5.8. Permanent deformations in wood-cement particleboard following impact The accelerometer voltage time histories for the steel ball impacting plain concrete, a wood-cement particleboard panel resting on concrete and a wood board resting on concrete are shown in Figures 5.9, 5.10 and 5.11, respectively. 112 . O . O o o ,::;2-.:f Agilent Technologies Figure 5.9 Voltage time history for impact on concrete I Agilent Technologies : l H=m ii A mm: = im: LLJ : i Figure 5.10 Voltage time history for impact WCPB resting on concrete 113 ~" Agilent Technologies Figure 5.11 Voltage time history for impact on wood board resting on concrete The conversion from voltage to acceleration is, 10.18 mV = 1.00 g where g = 9.81 m/sz. For the case of wood-cement particleboard resting on concrete, the accelerometer time histories are shown in Figure 5.12. 114 Acceleration, (g) ( Time, (ms) Figure 5.12 Acceleration time history of steel ball (W CPB on concrete) The velocity time histories were computed from acceleration time histories through integration. The time was assumed to be zero at initial impact when the acceleration exceeded that due to gravity. Since the ball was released from rest from a height of six inches (152.4 mm) above the impact target, the velocity of the ball, V, at initial impact can be computed using the conservation of energy: 1 , —mv‘ =m H 2 0 8 Solving for v0 yields v0 = ,/2gH =17.2 (m/second) 115 where m is the mass of the steel ball, g is the acceleration under gravity, and H =152 .4 mm. The velocity time histories are obtained through v(t) = v0 + £a(t)dt, t2 0 where v0 =17.2 m/s The velocity time history corresponding to the acceleration time history in Figure 5.12 is shown in Figure 5.13. _____.._,W___1 E E E . f . fl s: -2 2 4 6 8 .é‘ .8. l D l > 1 Time, (ms) Figure 5.13 Velocity time history of the steel ball (W CPB on concrete) 116 Similarly, the displacement time histories of the steel ball were obtained by integration of the velocity time histories. Defining the displacement at the top of the impact surface to be zero, the displacement time histories can be obtained by the following equation. do): Emma, with d(0)=0 The displacement time history corresponding to the velocity time history in Figure 5.13 is shown in Figure 5.14. ‘7 8 -6 -4 2 4 6 8 Time, (ms) AMT “BEMJC am”) i w T Figure 5.14 Displacement time history of the steel ball (W CPB on concrete) 117 Figure 5.15 compares the acceleration time histories of the steel ball impacting on wood—cement particleboard resting on concrete, concrete and wood board resting on concrete. 1 l 900 _ l 800 fi /Concrete 1 . 700 « | 600 “ l ’59 500 ~ 1 g 400 - g g 300 _ WCPB on concrete 1 .2 l 33 Wood on concrete ‘ < l r— -:.+ Wat,‘;.-_ ‘ ‘ b 1 Time, (ms) Figure 5.15 Acceleration time histories of steel ball impacting different surfaces In Figures 5.15, the maximum acceleration of 800g occurs when the steel ball impacts concrete. The peak acceleration for impact on WCPB is 220g and that for impact on the wood board is 180g. The deceleration forces on the steel ball due to impact on the WCPB and the wood board are close, while the deceleration force for impact on concrete is about four times greater. The wood-cement particleboard layer reduces the impact acceleration, and hence the maximum impact deceleration force, by about 72%. 118 Figure 5.16 and Figure 5.17 showed the velocity and displacement time histories of the steel ball for the three different cases shown in Figure 5.1. In Figure 5.16, the peak rebound velocities of the steel ball for impact on concrete, WCPB and wood are 1.2, 0.9 and 0.78 (mm/ms), respectively. Therefore, the wood-cement particleboard layer reduces the peak rebound velocity by 25%. In Figure 5.17, the peak negative displacements (maximum deformation of specimen due to impact) for impact on concrete, WCPB and wood are 0.6, 1.6 and 2.0 (mm), respectively. It is the large deformation of wood and WCPB that results in the reductions in peak acceleration and rebound velocity of the steel ball. Concrete -2 Velocity, (mm/ms) £- 1 Time, (ms) Figure 5.16 Velocity time histories of steel ball 119 Concrete WCPB Wood Displacement, (mm) Time, (ms) Figure 5.17 Displacement time histories of steel ball 5.3 Multi-Stress Test on Wood-Cement Particle Tube The multi-stress test was conducted by applying a compressive load on a wood- cement composite ring. The purpose of this test was to verify the accuracy of simulations (described later) to predict the response of wood-cement particleboard tubes under impact. The motivation for using tubes is presented in Chapter 7. In this research, the multi-stress test on the wood-cement particleboard ring was conducted to investigate the mechanical response of the ring. The WCPB ring was cut from a flat board with an outer diameter of 110 mm, inner diameter of 60 mm and thickness of 35 mm. The cement/wood ratio of the composite tube was 1.5. Figure 5.18 shows the geometry of the test specimen. Two test specimens were manufactured and tested. The ring was cut from a flat 35 mm thick WCPB. The fibers therefore randomly oriented in the plane of the ring. 120 (mm) 60 (mm) 35 mm 110 Figure 5.18 Geometry of specimen 5.3.1 Test results and analysis The compressive loading was applied using an MTS machine with a loading speed of 0.01 mm/second. Two displacement measurements were recorded at the top of the specimen’s external and internal circles as shown in Figure 5.19. The movement of the loading crosshead of the MTS machine was used as the displacement of the top of the test specimen. The loading direction was parallel to the cross section of the tube. The load-deformation curve was obtained in this test. The compressive test setup was shown in Figure 5.19. 121 Figure 5.19 Compression test setup The failure mode of the compression test is shown in Figure 5.20. The WCPB ring showed strong inelastic behavior. Even though the ring cracked and its shape deformed from a circle to an ellipse, it did not collapse. 122 Compressive load (N) Figure 5.20 Compressive failure of WCPB ring 4000 3500 r 3000 2500 r 2000 L 1500 1000 500 fi 7 Tfi 1 Q; L l Figure 5.21 0.5 1 1.5 2 2.5 3 Displacement (mm) Load-displacement curve for multi-stress test on WCPB ring 123 Figure 5.21 shows the relationship between the vertical load and the vertical displacement at the top of the specimen. The load-displacement curve indicates that the ring displays elastic-degrading plastic behavior. The behavior is elastic up to a load of 2800 N after which the ring undergoes stiffness degradation. Figure 5.22 shows the stress states at the points A and B and the stress distributions along the cross sections 1, II and III in the composite ring under vertical compressive load. The stress distributions explain the failure cracks observed in Figure 5.20. Figure 5.22 shows that the composite ring is in a multi-stress state under vertical compression loading. * .4 Figure 5.22 Stress state and stress distribution 124 5.4 Summary Results from a falling ball impact test shows that wood-cement particleboard possesses good energy dissipation characteristics. The reduction in the impact force when the steel ball impacts WCPB resting on concrete is similar to that for impact on a wood board resting on concrete. Compared with the steel ball impacting a concrete block, the wood-cement particleboard resting on concrete reduced the impact acceleration of the steel ball, and hence the maximum impact deceleration force, by about 72%. The ability of the WCPB to reduce such a large portion of the impact deceleration force suggests that WCPB has a strong potential to dissipate energy. The multi-stress test conducted on wood-cement particleboard ring samples showed that the rings display elastic-degrading plastic behavior similar to the behavior described in Section 3.3.3 for flexural specimens. 125 CHAPTER 6 VALIDATION OF MATERIAL MODEL FOR WOOD-CEMENT PARTICLEBOARD 6.1 Introduction Finite element simulation of the falling ball impact test was performed to validate the ability of the material models in LS-DYNA to adequately represent wood-cement particleboard and concrete. If the simulations is successful, then preliminary studies on the impact of a vehicle with a concrete crash barrier enhanced with wood-cement particleboard panels can be performed using finite element simulation. 6.2 Finite Element Modeling of Falling Ball Impact Test One of the important tasks in finite element simulation is finite element modeling. The quality of modeling directly affects to the accuracy of the results of the finite element simulation. The quality of modeling depends on many features, such as the power and flexibility of the modeling software, element modeling, material modeling, contact modeling and so on. 6.2.1 Modeling software In the simulation study, four commercial software packages were used. LS- DYNA (Hallquist, 1999) is used for the impact analysis. The description of LS-DYNA was presented in Section 2.13. HyperMesh (Altair Engineering, 1999) was used as a 126 preprocessor to develop the finite element model. HyperGraphic (Atair Engineering, 1999) and LS-POST (LSTC, 2002) were used for post-processing. LS-DYNA and LS- POST are the products of Livermore Software Technology Corporation. HyperMesh and HyperGraphic are the products of Altair Engineering, Inc. 6.2.2 Element modeling The steel ball, wood-cement particleboard and concrete were modeled with 8- node hexahedron solid elements. 6.2.3 Material modeling In nonlinear finite element analysis of vehicle-barrier crashes, the principal challenge is the capability of the material constitutive models to represent a realistic response of the barrier under impact loading. In this study, concrete, wood-cement particleboard and steel were modeled with the material models available in LS-DYNA. 6.2.3.1 Modeling concrete LS-DYNA offers several concrete material models, Material Model 16 (MAT_PSEUDO_TENSOR) is a model with the minimum required input data (Hallquist, 1999). Material Model 16 (MAT_PSEUDO_TENSOR) is a pseudo-tensor geological model with an option for reinforcement. The model offers two major modes: a simple pressure-dependent Mohr-Coulomb yield surface with the Tresca limit, and two “yield versus pressure” functions with the capability to transit from one curve to another. The 127 latter one is used with the damage scale option as suggested in the User Manual (Hallquist, 1999). The equation of state (EOS) type 8 is used, which describes the volumetric response of the material. In this study, two-yield surface versus pressure criteria were employed for modeling the concrete. Material Model 16 is based on the stress-strain relation of concrete under hydrostatic compression and a two yield surface limit. LS-DYNA uses a tri-linear relation between hydrostatic stress and volumetric strain to model the concrete behavior under hydrostatic compression. Figure 6.1 depicts the stress-strain relation adopted in LS- DYNA. :0 } Hydrostatic stress 0) l - 4 E Volumetric strain Figure 6.1 Hydrostatic stress vs. volumetric strain of concrete (schwer, 2001) The following algorithm for generating the default EOS (Equation of State) parameters is used to determine the pressure and volume strain pairs, and an associated unloading bulk modulus for each of the four points comprising the pressure-volume curve (Shewer, 2002). 128 Table 6.1 Equation of State Algorithrn for Generic Concrete (Shewer, 2002). 1’0”“ Bulk Unloading K...- Pressure I: Volume sum .9... 1 E/[3(1— 2v)] 0 0 2 120 f; 02/; —P, /KU, 3 300]: Be - Kuz (8v3 - £v2) .0068 4 Rs 'Ku3 (€124 —€v3) -010 The bulk unloading moduli are further modified to assure that the largest unloading modulus is associated with the last point of the curve: Km = max(KUl’KU3) Kw = Km (6.1) Kuz = KUl and then only the elastic Km and largest unloading moduli KU4 are retained in the generated EOS. The elastic modulus of concrete was estimated from the formula provided by the American Concrete Institute. The estimate of Young’s modulus for concrete, for a normal weight density of 145 lbf/ft3, is given by the formula E = 57,000,”; psi (6.2) and typical values of Poisson’s ratio for concrete range from 0.15 to 0.2. In this study, a Poisson ratio of 0.2 was used (Nilson, 1991). 129 LS-DYNA also uses the two-yield surface limit shown in Figure 6.2 as a failure criteria. In Figure 6.2, the lower curve represents the initial yield surface and the upper curve represents the evolution of the yield surface due to concrete hardening. P =a0+——— a1+azp Omax Yield \ afailed = 00f + alf-l-azp Pressure Figure 6.2 Yield stress vs. mean stress for concrete under hydrostatic compression The input parameters of the concrete material used in this study are given in Table 6.2. Table 6.2 Concrete Material Parameters Densi 2.4 cm Y ’s Modulus 21526 Poisson’s Ratio 0.2 've S 20 130 6.2.3.2 Modeling wood-cement particleboard Wood-cement particleboard is modeled as an isotropic material due to the small size of the wood particles. This simplifying assumption is used even though wood cement particleboard has directional properties. Material Model 24 (MAT_PIECEWISE_LINEAR_PLASTICITY) was selected to model wood-cement particleboard. Material Model 24 is suited for elasto-plastic material with an arbitrary stress-strain curve or tabulated stress-strain data (Hallquist, 1999). In this material model, the stress-strain pairs are taken from test data and failure is characterized by a maximum plastic strain limit. The stress-strain curve is defined by the effective stress and effective plastic strain. The effective plastic strain is a true plastic strain equal to the total strain minus the elastic strain, while the effective stress is the true stress corresponding to the effective plastic strain. Figure 6.3 shows a typical piecewise linear curve of effective stress vs. effective plastic strain. The piecewise linear curve defines the yield stress versus the effective plastic strain. A nonzero yield stress is defined when the plastic strain is zero. 131 “A .,//— Effective stress ’ Ep Effective plastic strain Figure 6.3 Effective stress vs. effective plastic strain curve (Hallquist, 1999). The engineering stress-strain curve does not give a true indication of the deformation characteristics of a material because it is based entirely on the original dimensions of the specimen, and these dimensions change continuously during the test. The true stress 0' is expressed in terms of engineering stress by a = s(e +1) (6.3) The true strain 8 may be determined from the engineering or conventional strain e g = ln (8 +1) (6.4) To find the curve of true stress and true plastic strain, three steps were taken. First, derive engineering stresses and strains, Engineering stress: 3 = i (6.5) 0 132 Strain Engineering strain: 8: L (6.6) 0 l l -3000 ~ 1 l l a i e l 8 a l (I) l l l l o i . . . . ; o -o.05 -o.1 -o.15 -o.2 t l Figure 6.4 Engineering stress vs. engineering strain (W CPB) Second, calculate the plastic strain, Plastic strain: Plastic strain cp = total strain (e) — elastic strain (cc) Le %= -——= - ’ (am where ep= plastic strain, sy = yield stress, Py = yield load, A0 = original cross section area, L0 = original length, and L = current length. 133 Third, using equation 6.3 and 6.4, calculate the effective stress (true stress) and effective plastic strain (true plastic strain) and make sure a nonzero yield stress is defined when the plastic strain is zero. Figure 6.5 shows the relation between effective stress and effective plastic strain. o L r . r T *F 0 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16 T fl Effoctlve plastic drain Figure 6.5 Effective stress vs. effective plastic strain (W CPB) Table 6.3 shows the input data required for the material model of wood-cement particleboard in this simulation. Table 6.3 WCPB Material Data Density 1.044 (g/crn ) Young’s Modulus* 400 (MPa) Poisson’s Ratio 0.2 Load curve Shown in Figure 6.5 Yield stress (compressive) 17.2 (MPa) Tensile cutoff stress 11.2 (MPa) _ _ * Young’s Modulus is in the direction perpendicular to the board thickness. 134 6.2.3.3 Modeling steel Steel material is ofien modeled with elastic, kinematic plastic or piecewise linear plasticity models. When the steel ball impacts the concrete block from 6 inches above the concrete, the maxiumum stress on the steel ball is well below the yield stress. Therefore, Material Model 1 (MAT_ELASTIC) was used to model the steel ball. The Materail Model 1 (MAT_ELASTIC) is a linear isotropic elastic material model (Hallquist, 1999). The material properties of the steel ball are listed in Table 6.4. Table 6.4 Material Data for Steel Ball Densi 7.85 cm Youn ’s Modulus 210 000 Poisson’s Ratio 0.2 Yield S 200 6.2.4 Contact modeling The contact-surface algorithm in LS-DYNA is a penalty-based method. In the falling ball impact simulation, there is one kind of contact interaction: steel ball to the surface of the particleboard for the steel ball impacting the particleboard panel resting on a concrete block, or steel ball to the surface of concrete for the steel ball directly impacting the concrete block. The contact algorithms are set as follows: 0 For the steel ball impacting the particleboard panel resting on a concrete block: 1). Set the particleboard’s top surface as the master surface and the surface of steel ball as a slave surface; 2) Set the top surface of the concrete block as master surface and the bottom surface of the particleboard as the slave surface. The 135 nodes on the slave surface cannot penetrate through the master surface. In LS- DYNA, the Surface to Surface contact type was used. 0 For the steel ball directly impacting the concrete block, set the top surface of concrete block as the master surface and the surface of the steel ball as a slave surface. The nodes on the slave surface cannot penetrate through the master surface. In LS-DYNA, the Surface to Surface contact type was used. 6.2.5 Boundary conditions In the impact tests, the impact ball falls fieely from a height of six inches (152.4 mm) above the impact target. Therefore, the initial velocity of the ball just prior to impact is 17.2 m/s. In addition, the constraint condition imposed on the concrete block is that the the nodes on the bottom of the concrete block are fixed as shown in Figure 6.6. Impact velocrtv Steel Ball Particleboard Concrete Constrained Figure 6.6 A h ILLUUVA (LIAM UVW‘M‘L‘J Wl‘ultions 136 6.2.6 Database output node In order to compare the simulation results with the test results, in the simulation model the results were output at a node at the exact location of the accelerometer mounted within the steel ball. The output node location is shown in Figure 6.7. Output node Figure 6.7 Output node location 6.2.7 Impact simulation and result anslysis Two types of impact simulations were conducted as described above. The finite element models for these simulations are shown in Figure 6.8. The simulations were carried out on a multi-processor Sun Unix workstation located in the Division of Engineering Computing Services in the College of Engineering at Michigan State University. 137 gnu II II ianll 1:: :i:,.-:: a. Ball impacting particleboard resting concrete b. Ball impacting concrete Figure 6.8 Finite element models All the following test and simulation results, such as accelerations, velocities and displacements, are in the vertical Z direction. Figure 6.9 shows the acceleration time histories of the steel ball from the impact test and simulation for impact on the concrete block. Figure 6.9 shows that the simualtion results have a very good agreement with the impact test results except that there is about a 7% difference in peak the acceleration between the test and simulation. The simulation results indicate that Mat__Pseudo_Tensor model can be effectively applied to model concrete material. Figure 6.10 shows the acceleration time histories of steel ball fi'om the impact test results and simulation for impact on WCPB resting on a concrete block. The figure shows that the simulation result matches the test result quite well, especially fi'om the impact point to the peak acceleration. But, in the simulation results, the accelerations following the peak acceleration display spurious oscillations. 138 The- spurious oscillations represent high fi'equency motions that the analysis model cannot acurately resolve and are mainly created by the algorithm of the analysis as well as the viscosity of the material. The explicit central difference method that is used in LS-DYNA does not automatically dissipate high frequency numerical oscillations. It is possible to use implicit time integration in LS-DYNA and this will dissipate the high frequency numerical oscillations. However, implicit time integration requires expensive iterative procedures that are time consuming and expensive. In practice, because a certain degree of spurious oscollation is not debilitating, employing explicit analysis and enforcing an artificial damping control to smooth the oscillations may be a good chice. In this falling ball problem, an explict analysis is applied and the spurious oscillations were controlled with the LS-DYNA control command Control-Bulk- Viscosity. The parameters used in the control command were the LS-DYNA recommended default values related to sound wave propagation in general elasto-plastic materials. In Figure 6.10, the spurious oscillations are limited and the simulation results match the test results quite well. In Figure 6.9, Figure 6.10, Figure 6.11 and Figure 6.12, t = 0 represents the moment the steel ball first touches the specimen’s top surface. The measured acceleration time history was shified in accordance with this. In Figure 6.12, the zero point in the displacement axis was defined at the specimen’s top surface. Negative displacement represents the deformations of the particleboard after the steel ball hits the board’s top surface in the downward direction. Figure 6.11 and Figure 6.12 show the velocity and displacement time histories from the impact test and simulation for impact on the WCPB resting on a concrete block, 139 respectively. The simulation results match the results from the impact test quite well and demonstrate that the nonlinear finite element analysis code LS-DYNA can effective simulate the impact test on the wood-cement particleboard and that the wood—cement particleboard and concrete can be modeled reasonably by the LS-DYNA elasto-plastic material model (MAT_PIECEWISE_LINEAR_PLASTICITY) and geological material model (MAT_PSEUDO_TENSOR), respectively. The conditions at t = O are therefore a(0) = g, v(0) = -l7.2 m/s, d(0) = 0. where a = acceleration, v = velocity, and d = displacement. 900 1 i 30° J’ g —— Impact Test 700 1 m 600 4‘ —— Simulation 500 J 400 -« 300 J 200 ‘ 1oo "gnomes-aw "x _ "7'“ w‘_,_ v-7— Y——vvvwm .4 -2 -100 o 2 4 6 8 (g) Acceleration, Time, (ms) Figure 6.9 Acceleration time histories from impact test and simulation for impact on the concrete block 140 Acceleration, (g) g; 8 L! . L4_J* \— Tirne, (ms) .. .r . i ll fury-"Pu rr (,7 wrigflnl . .- ,, ‘1“ .' “ 14: ‘i'lrir- ' J. 1'! I. ll" ww.‘ Impact test Simulation 10 12 Figure 6.10 Acceleration time histories from impact test and simulation for impact on WCPB resting on a concrete block L 2 Velocity, (mm/ms) Time, (ms) Impact test Simulation Figure 6.11 Velocity time histories from impact test and simulation (WCPB) 141 10 J -— Impact test ""'"" Simulation 81 61 -4 -2 10 12 Displacement (mm) M CD N z," __.L_e__< ‘ _ O) -1 CD 1 t“ Time, (ms) Figure 6.12 Displacement time histories from impact test and simulation (W CPB) 6.3 Finite Element Modeling of Multi-Stress Test In order to verify that the material model in LS-DYNA can be used to model wood-cement particleboard that is subjected to a multi-stress state, the finite element simulation of the multi-stress test on the WCPB tube was conducted. The software of LS- DYNA, Hypermesh, and LS-POST were used for simulation, preprocessing and post- processing, respectively. 6.3.1 Element modeling The wood-cement particleboard tube, loading cross head and supporting plate of the loading machine were modeled using 8-node solid elements. The finite element model is shown in Figure 6.13. 142 Loading crosshead Composite tube Supporting plate Figure 6.13 Finite element model 6.3.2 Material modeling The wood-cement particleboard tube was modeled with Material Model 24 (MAT_PIECEWISE_LINEAR_PLASTICITY). The loading crosshead and supporting plate of the loading machine were modeled with Material Model 1 (MAT_ELASTIC). 6.3.3 Contact modeling In the multi-stress test simulation, two contact interactions occurr between the loading machine and the testing specimen. As the composite tube deforms, the top and bottom surfaces of the composite tube contact with the surface of the loading crosshead and the surface of the supporting plate, respectively. The contact algorithms are set as follows: 143 0 Set the top surface of the composite tube as the slave surface and the surface of the crosshead as the master surface. The nodes on the slave surface cannot penetrate through the master surface. In LS-DYNA, the Surface to Surface contact type was used. 0 Set the bottom surface of the composite tube as the slave surface and the surface of the supporting plate as the master surface. The nodes on the slave surface cannot penetrate through the master surface. In LS-DYNA, the Surface to Surface contact type was used. 6.3.4 Boundary conditions In this simulation, there are two different boundary conditions consisting of the loading velocity and support conditions. The velocity condition was set to the loading speed of 0.01 mm/second, and fixity was imposed on the nodes along the bottom of the supporting plate. The boundary conditions are shown in Figure 6.14. lVelocity =0.01 min/second III'IIIIIII Constraintnodes “II-WIIIIIIII Figure 6.14 Boundary conditions 6.3.5 Database output node In order to compare the simulation results with the test results, the simulation results were output at the node on the top surface of the tube that has initial contact with the crosshead. The output node location is shown in Figure 6.15. Output node Figure 6.15 Location of output node 6.3.6 Multi-stress test simulation Figure 6.16 shows the largest deformation of the finite element model in the simulation. The shape of the deformed finite element model is close to the shape of the deformed test specimen in Figure 5.20. The deformed finite element model does not show cracks. Because LS-DYNA uses a Lagrangian formulation in which the mesh moves with the material, cracks are generally not introduced in the finite element model without special treatment. It is possible to utilize the DELETE command to make cracks occur. The DELETE command deletes any elements in which elemental stresses or strains exceed specified limits. However, in this research the focus was on the deformed shape and the load-displacement curve of the finite element model, and the DELETE 145 command was not employed in the simulation. It should be noted that the analysis properly accounts for failure of the material (i.e., cracks) by reducing the stiffness of failed elements. Therefore, although cracks are not visible, the analysis properly accounts for their presence. Figure 6.16 Deformed FE model Figure 6.17 shows the load-displacement curves obtained from the compressive test and the simulation. The simulation results match the compressive test results quite well. The simulation results indicate that the elasto-plastic material model (MAT_PIECEWISE_LINEAR_PLASTICITY) adequately models the wood-cement particleboard under a multi-stress state even though the material is truly orthotropic. 146 4000 3500 [ A 3000 IL Simulation E 2500 . (I) “g 2000 L 1000 l 500 r.’ O L l _l 1 AA. 0 O 5 l 1.5 2 2 5 3 Displacement (mm) Figure 6.17 Load—displacement curves from test and simulation 6.4 Summary The nonlinear, explicit, three-dimensional finite element analysis code LS-DYNA was applied to simulate a falling ball impacting a wood-cement particleboard resting on concrete block and a concrete block as well as the multi-stress test on a composite tube. The agreement between simulation results and experiments indicate that the nonlinear finite element analysis code, LS-DYNA, could be successfully used to simulate impact on wood-cement particleboard. The simulation results also indicated that the LS- DYNA material models MAT_PIECEWISE_LINEAR_PLASTICITY and MAT_ PSEUDO_TENSOR can be effectively employed to model wood-cement particle board and concrete, respectively. The simulation result of the multi-stress test indicates that although the WCPB is an orthotropic material, the isotropic plasticity model in LS- DYNA is able to provide very good results. 147 CHAPTER 7 FINITE ELEMENT SIMULATION OF VEHICLE CRASHING ON CONCRETE BARRIER ENHANCED WITH WCPB 7.1 Introduction Concrete crash barriers are designed to prevent vehicle passengers from injury and provide certifiable levels of vehicle containment. However, accident data shows that a large number of deaths still occur as a result of vehicles impacting concrete barriers. To improve roadside safiey it may be feasible to install energy absorbing devices to enhance the impact characteristics of existing concrete barriers so as to reduce injury to passengers. An enhanced barrier should be designed to absorb as much impact energy as possible so as to minimize the deceleration forces on vehicles in the case of vehicle impact and at same time maintain the integrity of the barrier. One approach is to install cushioning material on the side surface of concrete barriers. However, this kind of material should be durable and cost effective. Wood-cement particleboard is durable, cost effective and its use in high volume is favorable to the environment. The potential of using ECPB as cushioning material on concrete crash barriers is investigated in this chapter. The nonlinear, explicit, three dimensional finite element analysis code LS-DYNA was used to perform crash simulation of vehicle against a concrete barrier enhanced with wood-cement particleboard elements. The impact deceleration force was taken to be the key parameter related to occupant injury. The geometry of WCPB elements that was 148 attached to the sides of concrete crash barriers were varied to minimize the impact forces on the vehicle so as to reduce the risk of occupant injury during the crash. Three different wood-cement particleboard element geometries were considered: a flat board, a wave shape and bundles of tubes. 7 .2 Simulation Test Design and Evaluation Criteria 7.2.1 Concrete barrier A vertical concrete barrier was selected to conduct crash impact simulations. The compressive strength was taken to be 4000 psi. The barrier had a height of 1066 mm, a width of 190 mm and a length of 5000 mm. The longitudinal reinforcements consisted of six steel bars with a diameter of 15 mm, and the vertical stirrups were made of steel bars with a diameter of 8 mm at a spacing of 400 mm along the barrier’s longitudinal direction. Figure 7.1 shows the geometry of the concrete barrier and steel reinforcement. CD8 (1315 1 066 .‘.\ \V I 3 <1 Figure 7.1 Geometry of the concrete barrier and steel reinforcement 149 7.2.2 Enhanced concrete barrier The enhanced barrier contains a wood-cement particleboard facade installed on the side surface of the existing concrete barrier where impacts occur. Figure 7.2 shows the enhanced vertical concrete barrier with a flat wood-cement particleboard facade. The enhanced concrete barrier is expected absorb more impact energy and reduce the impact deceleration force on vehicles during impact. As both wood-cement particleboard and concrete belong to the family of cement- bonded composites, they have compatible properties and can be easily bonded with cement if necessary. However, it is proposed that the wood-cement particleboard facade be fastened using metal fasteners on the side surface of the concrete barriers. This installation will enable facades damaged by vehicle impacts to be replaced easily. Vertical Concrete barrier WCPB facade Figure 7.2 Enhanced vertical concrete barrier Three types of wood-cement particleboard facades were investigated. These consisted of a flat facade, a wave shape and bundled tubes. Figure 7.3 shows the cross the section of particleboard facades. 150 a. Flat Figure 7.3 Cross section of particleboard facades 7.2.3 Simulation test matrix In this study, frontal crash impact simulations were investigated. In order to find a suitable solution for using wood-cement particleboard facades to improve the impact characteristics of the existing concrete barrier, five different WCPB facades were investigated. The vehicle impact speed was 30 mph or 13.4 mm/ms and the total simulation time was set to 100 milliseconds. Table 7.1 shows the simulation matrix for the frontal crash impact studies presented herein. performed for different WCPB thickness and geometric parameters, and the ones b. Wave shape presented here yielded the best results. @©® c. Bundled tubes Table 7.1 Physical Properties of WCPB Facades A number of other studies were Double Triple Triple-tube Four-tube WCPB Shape Flat wave wave bundle bundle Thickness (mm) 35 35 25 25 25 Geometric =225 l=225 parameters (mm) h=60 h=60 r =112 r =76 151 7.2.4 Evaluation conditions and criteria The simulation conditions follow the guidelines in the National Car Assessment Program (NCAP) and the National Cooperative Highway Research Program Report 350 (NCHRP350). As NCAP recommends, the safety features of a vehicle were evaluated by a frontal crash on a rigid barrier at a velocity of 30 mph. The crashing vehicle model was the 820C that was recommended by NCHRP350. The 820C model represents a small car with a weight of 820 kg. The evaluation criteria used in these simulations are based on the acceleration of the vehicle during impact. The immediate causes of injury or death in traffic accidents are numerous, such as broken glass, fire, crushing of the vehicle, hurling of the passenger against the car, etc. However, a primary cause of injury is the acceleration a passenger experiences. The acceleration criteria used in this chapter are recommended in Information About Automobile Accidents (2003) and the Federal Motor Vehicle Safety Standard (FMVSS 214, 2000): 0 People can sustain an acceleration of 20g without injury. 0 People can tolerate accelerations up to 80g without serious injury. 0 Pelvic acceleration should be less than 130g for a survivable injury. 7.3 Finite Element Modeling The most difficult task in finite element simulation is finite element modeling. The quality of modeling directly affects the accuracy of the results of the finite element simulation. The quality of the modeling depends on many elements, such as software, element modeling, material modeling and so on. 152 In this simulation study, four commercial software packages were used. LS- DYNA was used for crash analysis, HyperMesh was used as a preprocessor to develop the finite element model, and HyperGraph and LS-POST were used for post-processing. 7.3.1 Element modeling The wood-cement particleboard and concrete were modeled with solid elements, and the steel reinforcement inside the concrete barrier was modeled with beam elements. The extremities of the beam elements were merged with the nodes of the solid elements. Thus, the reinforcement cannot debond from the concrete. In addition, it was assumed that no frictional sliding occurs between the particleboard and the concrete surface. The comer nodes of the elements for the particleboard were merged with the nodes of the elements for concrete. Figures 7.4 and Figure 7.5 show the element connections. Figure 7.6 shows the mesh for the steel bar inside the concrete barrier. Steel bar Concrete Concrete Figure 7.4 Concrete and steel bar elements Figure 7.5 WCPB and concrete elements 153 LEI _ r . kagm Steel bar inside concrete barrier Figure 7.6 Steel reinforcement meshed with beam elements 7.3.2 Material modeling In nonlinear finite element analysis of vehicle-barrier crashes, the principal challenge is the capability of the material constitutive models to represent a realistic response of the barrier under impact loading. In this study, concrete, wood-cement particleboard and steel bars were modeled with the material models available in LS- DYNA. 7.3.2.1 Modeling concrete Material Model 16 (MAT_PSEUDO_TENSOR) was used to model concrete material. The details of this material model were described in Chapter 6. The material parameters for the concrete are shown in Table 7.2 Table 7 .2 Concrete Material Parameters Density 2.4 (g/cm3) Young’s Modulus 21526 (MPa) Poisson’s Ratio 0.2 Com ressive Stren 20 MPa) 154 7 .3.2.2 Modeling wood-cement particleboard Material Model 24 (MAT_PIECEWISE_LINEAR_PLASTICITY) was selected to model the WCPB. As described in Chapter 6, the WCPB was assumed to be an isotropic material, which is an approximation. For elements in tension, failure was controlled with the modulus of rupture (or tensile strength). For elements in compression, the failure was controlled with the compressive strength. All input data for the wood- cement particleboard were exactly the same as the values used in Chapter 6 and are reported in Table 7.3. Table 7.3 WCPB Material Data TJeTrsity 1.044 (g/cm3) Young’s Modulus 400 (MPa) Poisson’s Ratio 0.2 Yield stress (compressive) 17.2 (MPa) Tensile cut off (MOR) 11.0 (MPa) * Young’s Modulus is in the direction perpendicular to board thickness. 7.3.2.3 Modeling steel Steel material is often modeled with elastic, kinematic plastic or piecewise linear plasticity models. Preliminary simulations in this study indicated that the maximum stress in the steel bars inside the concrete barrier was significantly lower than the yield stress. Therefore, Material Model 1 (MAT_ELASTIC) was used to model the steel reinforcement. Material Model 1 (MAT_ELASTIC) is a linear isotropic elastic material model (Hallguist, 1999). The material properties of the steel bar are listed in Table 7.4. 155 Table 7.4 Steel Bar Material Data Density 7.85 (g/cm3) Young’s Modulus 210,000 (MPa) Poisson’s Ratio 0.2 Yield Strenfl 200 (MPa) 7.3.3 Contact modeling The contact-surface algorithm in LS-DYNA is a penalty-based method as described in Chapter 6. In vehicle crash simulation, the contact interactions are much more complicated than in the falling ball impact problem modeled in Chapter 6. In vehicle crash simulations, there are three kinds of contact interactions: vehicle body to barrier surface, vehicle tires to the ground surface, and vehicle self contact (component to component and component self contact due to folding). The contact algorithms were set as follows: 0 For the contact interactions between vehicle and barrier surface, set barrier surface as master surface and vehicle surface at impacting side as a slave surface. The nodes on the slave surface cannot penetrate through the master surface. In LS-DYNA, use the Surface to Surface contact type. 0 For the contact between vehicle tires and the ground surface, set the ground surface as master surface, and the nodes on the tires as slave nodes. Use the Node to Surface contact type. 0 For vehicle self contact, specify that nodes on one component of the vehicle cannot penetrate through any other components of the vehicle. Use the Single Surface (self contact) contact type. 156 7.3.4 Vehicle model In this simulation study, a 1975 Honda Civic vehicle model (820C) was selected to conduct crash simulation. The 820C model was released to the public by the National Crash Analysis Center (NCAC). The 820C model has a weight of 820 kg and 5400 elements including shell elements, beam elements and solid elements. This vehicle model was built for frontal crash impact and angle impact. The Federal Highway Administration has approved the model for use in small vehicle traffic crash simulation studies. Figure 7.7 is the finite element model of the vehicle. Figure 7.7 Finite element model of the1975 Honda Civic (820C) 7.3.5 Center of gravity of vehicle In most car vehicles, the center of gravity (CG) of the car is located between the two frontal seats and about 100 to 300 mm above vehicle’s floor. In this vehicle model, 157 its center of gravity is between the two frontal seats and 273 mm above the vehicle’s floor or 57 8 mm above the ground. In order to record the vehicle’s impact response, an accelerometer was mounted at the center of gravity of the vehicle. Accelerations, velocities and displacements of the vehicle were output from the accelerometer. Figure 7.8 shows the location of the center of gravity and accelerometer. Figure 7.8 CG and accelerometer location 7.3.6 Boundary conditions Two kinds of boundary conditions were imposed in the crash simulation. One boundary condition is the impact velocity of the vehicle. In this frontal crash impact simulation, the impact velocity of the vehicle was 30 mph or 13.4 mm/ms. The impact velocity was imposed on all nodes of the crash vehicle. 158 Another boundary condition is the constraint condition imposed on the concrete barrier and the ground. The bottom of the concrete barrier and the ground are fixed. Therefore, all nodes at the bottom of the concrete barrier and on the ground elements were fixed in x, y and 2 directions. Figure 7.9 shows the boundary condition. Velocity = 30 mph ' Constrained nodes Figure 7.9 Boundary conditions of the FE model 7.4 Finite Element Simulation As shown in Table 7.1, six different types of frontal vehicle-barrier crash simulations were conducted. In each crash event, the deceleration force on the vehicle during impact is the most important because this correlates with the severity of occupant injuries. To significantly reduce the deceleration force on the vehicle, the wood-cement particleboard elements must dissipate a large amount of impact energy by undergoing large deformations. Concrete barriers enhanced with wood-cement particleboard 159 elements having different geometric configurations were studied to determine which configuration is most effective in reducing impact forces. 7.4.1 Frontal crash set up Six different types of frontal crash simulations with different enhanced barriers were conducted using LS-DYNA. These included crash on (1) a plain concrete barrier and crashes on the concrete barrier enhanced with WCPB facades having (2) flat, (3) double-wave shape, (4) triple-wave shape, (5) triple-tube bundle, and (6) four-tube bundle facade, respectively. The finite element models of the six different frontal crash simulations are shown in Figures 7.10 to 7.15. a. are, . /"v”//// 47/ ‘ ' I I ”’05: Figure 7.10 Concrete barrier 160 Figure 7.11 Concrete barrier with flat WCPB facade ////// "'I ///// ”ff/g,” "I”: III/”I’ll,” If], 1:55.: Figure 7.12 Concrete barrier with double-wave WCPB facade 161 x/. // /// 244/4 3937 / / I l/l/II/l/l/Ill: .. 40? s ‘l -“ \‘II ‘ New“? Figure 7.13 Concrete barrier with triple-wave WCPB facade Figure 7.14 Concrete barrier with triple-tube bundle WCPB facade 162 . ‘l . §‘- ~ . 9.! Figure 7.15 Concrete barrier with four-tube bundle WCPB facade 7.4.2 Simulation results The nonlinear, explicit, three-dimensional finite element simulation for a vehicle barrier crash creates two major types of outputs that include XY pair data and graphic images of vehicle—barrier crash at every time step. For the analysis presented here the time step was taken to be one millisecond. Figure 7.16 to Figure 7.21 show the 820C vehicle crashing on a plain concrete barrier, and a concrete barrier with each of the five WCPB facades shown in Figure 7.11 to 7.15. Each figure shows snapshots at five different time steps: t = 0, 10, 30, 70 and 100 (ms). The crash characteristics at each of these time steps are as follows: 163 t = 0 ms: time step just before the vehicle impact the barrier. t = 10 ms: time at which the frontal bumper is deformed to its maximum level and just before the vehicle’s fi'ontal head contacts with the barrier. t = 30 ms: time at which the vehicle’s deceleration force reaches the maximum value. t = 70 ms: time at which the vehicle just loses contact with the barrier. t = 100 ms: time at end of the simulation. The characteristics described above do not occur exactly at the indicated times (t=10, 30 and 70 ms) for all cases but occurs within 1 or 2 millisecond of these times. It should be noted that the facades do not appear deformed in Figures 7.18 to 7.21 because the cross section of the facades and barriers shown are outside the impact region. 164 t=0ms Figure 7.16 Crash on concrete barrier Figure 7.17 Crash on flat WCPB facade 165 t=0ms 10ms t t=30ms = 70 ms t t=100ms Figure 7.19 Crash on triple-wave Figure 7.18 Crash on double-wave WCPB WCPB facade facade 166 t=0ms 10 ms t =30ms t =70 ms t 100 ms t Figure 7.21 Crash on four-tube WCPB 20 Crash on triple-tube WCPB Figure 7 facade facade 167 Figure 7.22 to Figure 7.27 show the damage on the vehicle at t = 70 ms for impact against different barriers. Figure 7.22 Vehicle damage after crash on concrete barrier (at t = 70 ms) Figure 7.23 Vehicle damage after crash on flat WCPB facade (at t = 70 ms) 168 Figure 7.24 Vehicle damage after crash on double-wave WCPB facade (at t = 70 ms) Figure 7.25 Vehicle damage after crash on triple-wave WCPB facade (at 70 ms) 169 Figure 7.26 Vehicle damage after crash on triple-tube WCPB facade (at t = 70 ms) \\\\\\ \\ \\'\“\\\\\\\:‘, \S‘ \\ \\\\ \\\‘\\\“‘ Figure 7.27 Vehicle damage afier crash on four-tube WCPB facade (at t = 70 ms) 170 These figures show the damage to the vehicle for each different crash case. These are two noticeable characteristics in Figure 7.16 to 7.27: one is the upward lift of the vehicle’s rear lift; another is the appearance of the vehicle damage. The simulation results show that upward lift of the rear wheel ends and the appearance of external damage vary from one to another. However, the appearance of the external damage is clearly related to the barrier’s geometric configuration. The flatter the contact surface of the barrier, the better the vehicle looks after impact. For good energy absorption, the facade’s height should cover the height from the bottom of the bumper to the top of the vehicle’s frontal head. The plain concrete barrier and concrete barrier with the flat WCPB facade provide similar damage to the vehicle after impact than the other four types of facades. The appearance of the damaged vehicle was the worst for the concrete barrier enhanced with double-wave WCPB facade (Figure 7.18 and Figure 7.24). This was because the height of the WCPB panel was smaller than the height of the vehicle’s frontal head. In Figure 7.18, the double-wave WCPB facade only covers the bumper. The lower part of the vehicle’s frontal head impacted the WCPB facade, whereas the upper part impacted the concrete part of the barrier, thereby causing the worst damage appearance to the vehicle’s head. The acceleration, velocity and displacement time histories at the center of gravity of the crashing vehicle for the six different barrier types described in Table 7.1 are shown in Figure 7.28, Figure 7.29 and Figure 7.30, respectively. 171 300 , Double wave 250 *- . Triple-tube E 200 . Hg Four-tube v ‘ . \\ Triple-wave/ \r‘ E “‘\R.°°"~..... a) 150 ‘4 \r . '0... g ' Concrete x- l -5 0. "g. 100 ‘ Flat \\ .52 Q 50 - 0 T I l l 0 20 40 60 80 100 Time (ms) Figure 7.28 Displacement time histories of vehicle 14 l Triple-tube 12 j Double wave Velocity (mm/ms) O) 4 1 ‘ \ » Four-tube 2 4, Triple-wave—A,‘ 0 IL I T T r \‘o. \ F\ r -2 5 1o 15 2o 25 ' .4 _6 I Time (ms) Figure 7.29 Velocity time histories of vehicle 172 Acceleration (g) Four-tube —'~" 1, ~ '° \ ‘. o '100 i Triple-wave r" \ -120 ~ Concrete Figure 7.30 Acceleration time histories of vehicle In Figure 7.28, the largest displacement occurs for impact on the triple-tube and four-tube facades, and the smallest displacement occurs for impact on the plain concrete barrier and the flat WCPB facade. In Figure 7.29, the vehicle impacting the tube facades required more time to reach zero velocity than that in the other four cases. This indicates that the tube facades experienced larger deformation, dissipated more impact energy, and were more effective in moderating the impact forces on the vehicle. The vehicle decelerations during impact are shown in Figure 7.30. Localized peaks appear in two groups: when the vehicle’s bumper contacts the barrier and when the full vehicle head contacts the barrier. In the first group of localized peaks (between 5 and 10 ms), the deceleration for impact on the concrete barrier reaches the maximum value at a time of about 8.5 milliseconds. The deceleration for impact on the flat WCPB facade is essentially identical to that for impact on the concrete barrier. For the double-wave and triple-wave facades, 173 the accelerations are essentially identical in the first group of localized peaks, and the maximum values are 70% lower than that for impact on the concrete barrier. For impact on the tube facades, there is no obvious maximum in the first group. In the second group of localized peaks (between 22 and 26 ms), the maximum decelerations for the flat, triple-wave, four-tube and triple-tube facades were reduced by 7%, 9%, 20% and 30%, respectively, compared to the maximum deceleration for the concrete barriers. For impact on the double-wave facade, however, the maximum deceleration increased by 8% compared to that for impact on the concrete barrier. It is evident that the geometric configuration of the particleboard facade has a significant influence on the energy absorbing behavior of the enhanced barrier. The simulation results show that with a good geometric configuration of the particleboard facade it is possible to reduce the peak deceleration by 30%. The presence of a bumper on the vehicle makes its impact on the flat WCPB facade somewhat different from the impact of the steel ball studied in Chapter 5. The steel ball was quite rigid and even a flat WCPB facade was able to reduce the maximum deceleration compared to impact on plain concrete. However, in the vehicle the bumper absorbs most of the energy, especially during the early phase of the impact. This is why in the first group of localized peaks, which represents collision of the bumper, the maximum accelerations for impact on the flat WCPB facade and the plain concrete barrier are essentially identical. In the second group of localized peaks, which represent collision of the more rigid frontal head of the vehicle, there is a slight reduction in the maximum deceleration for impact on the flat WCPB facade compared to impact on the 174 plain concrete barrier. However, the decrease of 7% is still much smaller than the 72% reduction observed for the steel ball in Section 5.2. The results indicate that the triple-tube facade absorbs the most energy amongst the configurations considered and consequently generates the lowest deceleration forces that the vehicle passengers have to withstand during impact. The triple-tube facade is most effective because it deforms the most as shown in Figure 7.31. 3-tube panel Figure 7.31 Deformation of triple-tube facade after impact As mentioned in Section 7.2.4, passengers in vehicles can tolerate a maximum acceleration of 80g during impact without serious injury. The deceleration on passengers should be smaller than the deceleration of the vehicle during impact because there is relative movement between the vehicle and passengers. In this simulation, for the vehicle impacting the three-tube facade the deceleration was 80g and the passengers inside this vehicle should therefore experience decelerations smaller than 80g and not be subjected to serious injury. 175 7 .4.3 Comparison of WCPB, concrete and steel triple-tube facades To further investigate the contribution of the shape and material of the tube facade in reducing the impact acceleration, crash simulations onto a concrete barrier enhanced with a triple-tube facades made of steel and concrete were conducted. The geometry of the concrete triple-tube facade was the same as that of the WCPB triple-tube facade. For the steel triple-tube facade, two cases were studied with each tube having the same outer diameter as that of the WCPB tube but with thicknesses of 3 mm and 5 mm. Figure 7.32 to Figure 7.35 show the crash images at the largest tube deformation for each case. As evident, in these figures, the WCPB facade has modest deformation (maximum displacement in vehicle moving direction = 32 mm), the concrete tube facade has very little deformation due to its rigidity (maximum displacement in vehicle moving direction = 1.2 mm), and the 3 mm thick steel tubes have very large deformation because of its high flexibility (maximum displacement in vehicle moving direction = 220 mm), and the 5 mm thick steel tubes deform more than the WCPB tubes but less than 3mm thick steel tubes (maximum displacement in vehicle moving direction = 123 mm). 176 Figure 7.32 Vehicle crashing on WCPB triple-tube facade Figure 7.33 Vehicle crashing on concrete triple-tube facade 177 Figure 7.34 Vehicle crashing on 3 mm thick steel triple-tube facade Figure 7.35 Vehicle crashing on 5 mm thick steel triple-tube facade 178 3 mm thick steel tubes Concrete ' " . -80 _ tubes / '. 5 mm thick steel tubes Acceleration (g) 40° i WCPB tubes 11,, -120 l ‘J _140.rs Figure 7.36 Acceleration time histories of vehicle for four triple-tube facades Figure 7.36 shows the acceleration time histories at the center of gravity of the crashing vehicle for the various types of triple-tube facades, the peak acceleration for concrete triple-tube facade is 120g, which is almost the same as the acceleration of the vehicle that impacts a plain concrete barrier. Therefore, the concrete tube facade does not improve the impact characteristics of the modified concrete barrier. The peak accelerations for the two steel triple-tube facades are 65g and 68g for the 5 mm and 3 mm thicknesses, and are lower than the peak acceleration for the WCPB triple-tube facade (80g). While steel performs better than WCPB, the WCPB performs adequately, is cheaper, and its use promotes environmental conservation. Figure 7.36 indicates that both the shape as well as the energy absorption characteristics of the material affect the performance of the facade. 179 7.5 Summary Large deformation, dynamic nonlinear finite element analysis was used to evaluate the performance of a concrete barrier enhanced with five different wood-cement particleboard facades subjected to vehicle impact. The results of the analysis indicate that it is possible to improve the energy absorption capability of a concrete crash barrier by adding appropriately configured wood-cement particleboard facades. The simulation results indicate that the triple-tube facade reduces the deceleration forces on the vehicle the most. For a frontal impact of a Honda Civic vehicle traveling at 30 mph, the triple-tube WCPB facade reduces the vehicle deceleration during impact to 80g compared to 120g when no facade is used. Occupants of vehicles sustain serious injuries when the deceleration during impact exceeds 80g. Therefore, the use of the triple-tube WCPB facade can prevent serious injury to vehicle occupants during a frontal impact at 30 mph. Comparisons of the performance of WCPB, concrete and steel triple-tube facades indicate that although the steel tubes are most effective in reducing the deceleration forces, the WCPB tubes also perform quite well, while the concrete tubes are ineffective. 180 CHAPTER 8 CONCLUSIONS 8.1 Introduction The work reported in this dissertation include a new manufacturing process for making high performance wood-cement particle composites, material characterization of the composites subjected to bending, compression and impact loading, and results of dynamic large deformation nonlinear finite element analysis for simulating impact tests on wood-cement particleboard and simulating a vehicle impacting a concrete barrier enhanced with wood-cement particleboard facades. Background information about wood-cement composites and computational simulation of a vehicle impacting traflic crash barriers also is provided. The most significant findings of this study as well as a discussion of experimental and analytical future research that will advance this research further are summarized in this chapter. 8.2 Development of Wood-Cement Particleboard 8.2.1 Manufacturing process A new process for manufacturing wood-cement particleboard is presented and consists of pressure control and fully saturated curing to produce high-performance wood-cement particleboard. In particular, the fully saturated curing procedure improves the bonding between the irregular surface of wood particles and the cement matrix. As 181 a result, the bending strength of wood-cement particleboard reaches 11.7 MPa and is higher than the cormnonly accepted limit to 10 MPa (Wolfe, 1996). 8.2.2 Effect of cement/wood ratio to bending strength Bending tests were performed to establish the relationship between bending strength and the cement/wood ratio. The particleboard with a cement/wood ratio of 1.5 yields the maximum bending strength (or modulus of rupture) and may be considered as the optimum cement/wood ratio. The results also indicate that the bending strength of WCPB increases as the cement/wood ratio increases from 1.0 to 1.5 and decreases when the cement/wood ratios increases further from 1.5 to 4.0. The test results also indicate that the modulus of elasticity and density of the particleboard increases almost linearly as the cement/wood ratio increases. The toughness index of 6.0 achieved from bending tests indicates that the wood-cement particleboard has a higher energy dissipation capacity compared to steel fiber reinforced concrete which has a toughness index of 5.0. Therefore, the wood—cement particleboard can be used when energy dissipation is desired. 8.2.3 Compressive properties The compressive load-deformation curve of WCPB displays significant softening non-linearity indicating that the material has the capability to absorb energy. The material properties of WCPB are not isotropic but have directional dependencies due to the 182 orientation of the wood particles resulting from pressing during the manufacturing process. Short column specimens failed predominantly in shear under compressive loading irrespective of the orientation of the particles in the columns. The test results indicated that WCPB with a cement/wood ratio of 1.5 exhibited a compressive strength comparable to that of normal concrete. However, the strain at peak load was ten to fifty times larger than that of normal concrete depending on the direction of the compressive loading. The ability to sustain such large deformations implies that WCPB can be used for applications where energy dissipation is desired. A WCPB tube was also tested under compressive loading applied along a diameter. The test results indicated that the tube had a large plastic deformation. Under a multi-stress state the wood-cement particleboard can also be modeled as an elasto-plastic material. 8.2.4 Impact characteristics A falling ball impact test was used to study the impact characteristics of WCPB. The falling ball impact test was performed on a plain concrete block, WCPB resting on the concrete block, and a wood board resting on the concrete block. The time histories of acceleration, velocity and displacement for impact on WCPB are much closer to the corresponding time histories for impact on the wood board rather than for impact on plain concrete. The wood-cement particleboard resting on concrete reduced the maximum impact deceleration force by about 72% compared to the deceleration force for impact on 183 concrete. The ability of the WCPB to reduce the impact deceleration force by such a large amount suggests that WCPB has a strong potential to dissipate energy. 8.3 Computational Simulations of Impact on Wood-Cement Particleboard Simulation results indicate that the nonlinear finite element analysis code, LS-DYNA, can be successfully applied to simulate the mechanical tests on wood-cement particleboard. The simulation results agree very well with the results of both the impact test and multi-stress test. The simulation results also indicate that the LS-DYNA material models could be effectively applied to model the concrete and wood-cement particleboard. The simulation results further indicated that the wood-cement particleboard displays elastic-degrading plastic behavior under a multi-stress state and assuming that the WCPB is an isotropic elasto-plastic material in finite element analysis produces reasonable results even though the real material has directional properties. Dynamic nonlinear finite element analysis was applied for evaluating the designs of a concrete crash barrier enhanced with wood-cement particleboard facades subjected to vehicle impact. The results of the simulations indicate that it is possible to maximize the energy absorption ability of the system by selecting an appropriate geometric configuration for the wood-cement particleboard facade. The concrete barrier enhanced with triple-tube WCPB facade provides the highest level of crash energy absorption. The 184 geometry of the concrete barrier enhanced with the triple-tube wood-cement particleboard facade assures controllable deformations and reduces the potential injury to vehicle occupants. 8.4 Future Research Future research, development, and applications of wood-cement particleboard are necessary in order for enhanced concrete crash barriers with WCPB facade to become a reality. The future works to study include the development of: 0 Better protective coating system (fiber-resin coating or resin coating) for WCPB facade to strengthen its durability under freeze-thaw. 0 Better material model to accurately characterize the material properties of wood-cement particleboard. 0 Optimization of the geometric configuration of wood-cement particleboard facade used to enhance concrete crash barriers. 0 Development of connection details for securing the WCPB facade to the concrete barriers. Because of the complexity of the behavior of concrete barriers enhanced with the triple-tube WCPB facade, a field crash test of a vehicle impacting an enhanced concrete crash barrier is also recommended in the future research. 185 APPENDICES 186 APPENDIX A AN 820C VEHICLE IMPACTING A CONCRETE BARRIER ENHANCED WITH A 3-TUBE WOOD-CEMENT COMPOSITE PANEL This appendix presents the input file of an 820C vehicle impacting a concrete barrier enhanced with a 3-tube wood-cement particle panel. For simplification, the original 596 pages input file was simplified into current input file. The current input file only presents the major command syntax but eliminating most of the data related to Nodes and Elements. The input file is in keyword format in LS-DYNA Version 960 and generated using HyperMesh Version 5.1 and Text Editor as well. ‘KEYWORD I"TITLE 820C VEH IMPACT SIMULATION WITH VERTICAL CONCRETE BARRIER ENHANCED WITH WCPB $$ HM_OUTPUT_DECK created 18:06:59 12-10-2003 by HyperMesh Version 5.1 $5 Generated using HyperMesh-Ls-dyna Template Version : 5.0-l *CONTROL_TERMINATION $$ ENDTIM ENDCYC DTMIN ENDENG ENDMAS 100.0 0 0.0 0.0 0.0 ‘CONTROL_TIMESTEP $$ DTINIT TSSFAC lSDO TSLIMT DTZMS LCTM MSIST 0.00.89999998 0 0.0 -0.00111 0 l *CONTROL_SHELL SS WRPANG ITRIST IRNXX ISTUPD THEORY BWC PROJ 45.0 2 -1 0 2 2 l *CONTROL_HOURGLASS $$ [HO OH 5 0.1 *CONTROL_BULK_VISCOSITY $5 Q2 Q1 1.5 0.06 *CONTROL_CONTACT $3 SLSFAC RWPNAL ISLCHK SHLTHK PENOPT THKCHG ENMASS 0.1 0.0 2 O 1 0 1 187 ERODE MITER ORIEN $$ USRSTR USRFRC NSBC S INTERM XPENE SSTHK ECDT TIEDPRJ 0 0 0 0 0.0 0 0 0 *CONTROL_PARALLEL $$ NCPU NUMRHS ACCU 4 0 1 *CONTROL_COUPLIN G $5 UNLENG UNTIME UNFORC TIMIDL FLIPX FLIPY FLIPZ SUBCYL l .0 1 .0 0.0 0.0 0 0 0 l ’CONTROL_OUTPUT $5 NPOPT NEECHO NREFUP IACCOP OPIFS IPNINT IKEDIT l 3 0 0 0.0 0 100 0 *CONTROL_ENERGY $$ HGEN RWEN SLNTEN RYLEN 2 2 2 2 $$DATABASE_OPTION -- Control Cards for ASCII output *DATABASE_NODOUT 1.0 *DATABASE_GLSTAT 1.0 *DATABASE_MATSUM 1.0 *DATABASE_RBDOUT 1.0 *DATABASE_BINARY_D3PLOT $5 DT/CYCL LCDT BEAM NPLTC 2.0 0 0 0 *DATABASE_BINARY_D3THDT $$ DT/CYCL LCID 2.0 0 *DATABASE_BINARY_D3DUMP $8 DT/CYCL 40000.0 *DATABASE_BINARY_RUNRSF $5 DT/CYCL 10000.0 *NODE l 67 1 .50823 85485 -767.1 162518609266499999970496 *MAT_ELASTIC 188 $HMNAME MATS 1MAT1_1 11.0120E-O7 200.0 0.33 0.0 *MAT_ELASTIC $HMNAME MATS 3MAT1_3 38.1280E-O6 200.0 0.33 0.0 ‘MAT_ELASTIC SHMNAME MATS 4MAT1_4 42.2000E-06 80.0 0.33 0.0 *MAT_ELASTIC $HMNAME MATS 5MAT1_5 52.2000E-O6 80.0 0.33 0.0 ’MAT_ELASTIC $HMNAME MATS 6MAT1_6 68.1140E-O6 200.0 0.33 0.0 *MAT_ELASTIC $HMNAME MATS 8MAT1_8 81 .897OE-06 200.0 0.33 0.0 *MAT_ELASTIC $HMNAME MATS 20MAT1_20 207.86OOE-06 200.0 0.33 0.0 *MAT_ELASTIC SHMNAME MATS 21MAT1__21 217.8600606 200.0 0.33 0.0 ‘MAT_ELASTIC $HMNAME MATS 22MAT1_22 227.8600606 200.0 0.33 0.0 *MAT_ELASTIC SHMNAME MATS 24MAT1_24 241 .0120E-07 200.0 0.33 0.0 *MAT_ELASTIC SHMNAME MATS 26MAT1__26 262.7780608 200.0 0.33 0.0 *MAT_PLASTIC_KINEMATIC SHMNAME MATS 2MAT3_2 27.8600606 200.0 0.33 0.207 0.0 0.0 0.0 0 ‘MAT_PLASTIC_KINEMATIC SHMNAME MATS 7MAT3_7 77.8600606 200.0 0.33 0.207 0.0 0.0 0.0 0 *MAT_PLASTIC_KINEMATIC 189 SHMNAME MATS 9MAT3_9 938000607 10.0 0.35 0.0207 0.1 0.0 0.0 0.0 0 *MAT_PLASTIC_KINEMATIC $HMNAME MATS 10MAT3_10 105.6050607 200.0 0.33 0.207 2.0 0.0 0.0 0.0 o *MAT_PLASTIC_KINEMATIC $HMNAM6 MATS rrMAT3__11 117.8600E-06 200.0 0.33 0.207 2.0 0.0 0.0 0.0 o *MAT_PLASTIC_KINEMATIC $HMNAME MATS 12MAT3_12 1278600606 200.0 0.33 0.207 2.0 0.0 0.0 0.0 0 *MAT_PLAST1C_KIN6MATIC SHMNAME MATS 13MAT3_13 135.7410607 30.0 0.33 0.02 0.03 0.0 0.0 0.0 0 ‘MAT_PLASTIC_KINEMATIC $HMNAME MATS 14MAT3_14 1478600606 200.0 0.33 0.207 2.0 0.0 0.0 0.0 0 *MAT_PLASTIC_KINEMATIC $HMNAM6 MATS 15MAT3_15 1578600606 200.0 0.33 0.207 2.0 0.0 0.0 0.0 0 *MAT_PLASTIC_K1N6MATIC SHMNAME MATS 17MAT3_17 1778600606 200.0 0.33 0.207 2.0 0.0 0.0 0.0 0 *MAT_PLAST1C_K1N6MAT1C SHMNAME MATS 18MAT3_18 1878600606 2000.0 0.33 2.07 2.0 0.0 0.0 0.0 0 *MAT_PLASTIC_KINEMATIC $HMNAME MATS 19MAT3_19 1978600606 200.0 0.33 0.207 2.0 0.0 0.0 0.0 0 *MAT_PLASTIC_KINEMATIC $HMNAME MATS 23MAT3_23 190 237.8600E-06 200.0 0.33 0.207 2.0 0.0 0.0 0.0 0.0 0 *MAT_PLASTIC_KINEMATIC $HMNAME MATS 25MAT3_25 251.5720605 200.0 0.33 0.207 2.0 0.0 0.0 0.0 0.0 0 *MAT_NULL SHMNAME MATS lOZNULL 1024.0000607 200.0 *MAT_RIGID $HMNAME MATS 16MAT20_16 161.4650E-06 200.0 0.33 0.0 0.0 0.0 1.0 0 0 0.0 0.0 0.0 0.0 0.0 0.0 *MAT_PIECEWISE_LINEAR_PLASTICITY $HMNAME MATS 108board 1081 .0400E-06 0.37 0.3 0.017 0 0 $$ HM Entries in Stress-Strain Curve = 8 0.0034 0.0068 0.0096 0.0123 0.0146 0.0178 0.0188 0.0 0.01 0.02 0.033 0.0475 0.0808 0.1168 *MAT_RESULTAN T_PLASTIC1TY SHMNAME MATS 101MAT_BAR 1017.8340E-06 200.0 0.33 0.207 0.0 I"PART SHMNAME COMPS lPartl SHMCOLOR COMPS 1 1 material type # 1 (elastic) l 1 l 0 0 0 *PART SHMNAME COMPS 2Part2 $HMCOLOR COMPS 2 2 material type # 3 (Kinematic/Isotropic elastic-plastic) 2 2 2 0 0 0 1"PART SHMNAME COMPS 3Part3 SHMCOLOR COMPS 3 3 material type # l (elastic) 3 3 3 O 0 0 *PART SHMNAME COMPS 4Part4 191 0.0142 0.151 0.3 SHMCOLOR COMPS 4 4 material type # 1 (elastic) 4 4 4 0 ‘PART $HMNAME COMPS 5Part5 SHMCOLOR COMPS 5 5 material type # l (elastic) 5 5 5 0 ‘PART SHMNAME COMPS 6Part6 SHMCOLOR COMPS 6 6 material type # 1 (elastic) 6 6 6 0 *PART SHMNAME COMPS 7Part7 $HMCOLOR COMPS 7 7 material type # 3 (Kinematic/Isotropic elastic-plastic) 7 7 7 0 ‘PART SHMNAME COMPS 8Part8 $HMCOLOR COMPS 8 8 material type # l (elastic) 8 8 8 0 "PART $HMNAME COMPS 9Part9 $HMCOLOR COMPS 9 9 material type # 3 (Kinematic/Isotropic elastic-plastic) 9 9 9 0 ‘PART SHMNAME COMPS lOParth SHMCOLOR COMPS 10 10 material type # 3 (Kinematic/Isotropic elastic-plastic) 10 10 10 0 *PART SHMNAME COMPS llPartll SHMCOLOR COMPS ll 11 material type # 3 (Kinematic/Isotropic elastic-plastic) ll 11 ll 0 ’PART $HMNAME COMPS 12Part12 SHMCOLOR COMPS 12 12 192 material type # 3 (Kinematic/Isotropic elastic-plastic) 12 12 12 0 *PART SHMNAME COMPS 13Part13 $HMCOLOR COMPS 13 13 material type # 3 (Kinematic/Isotropic elastic-plastic) 13 13 13 0 *PART $HMNAME COMPS l4Part14 $HMCOLOR COMPS l4 l4 material type # 3 (Kinematic/Isotropic elastic-plastic) l4 14 14 0 *PART $HMNAME COMPS lSPartlS SHMCOLOR COMPS 15 15 material type # 3 (Kinematic/Isotropic elastic-plastic) 15 15 15 0 *PART SHMNAME COMPS 16Partl6 $HMCOLOR COMPS 16 1 material type # 20 (Rigid) l6 l6 l6 0 *PART $HMNAME COMPS 17Part17 SHMCOLOR COMPS 17 1 material type # 3 (Kinematic/Isotropic elastic-plastic) 17 l7 17 0 *PART $HMNAME COMPS 18Part18 SHMCOLOR COMPS l8 2 material type # 3 (Kinematic/Isotropic elastic-plastic) 18 18 18 0 *PART $HMNAME COMPS 19Partl9 $HMCOLOR COMPS 19 3 material type # 3 (Kinematic/Isotropic elastic-plastic) 19 19 19 0 *PART SHMNAME COMPS 20Part20 SHMCOLOR COMPS 20 4 material type # l (elastic) 193 20 20 20 0 ‘PART $HMNAME COMPS 21Part21 SHMCOLOR COMPS 21 5 material type # l (elastic) 21 21 21 0 *PART SHMNAME COMPS 22Part22 SHMCOLOR COMPS 22 6 material type # l (elastic) 22 22 22 0 I"PART $l-IMNAME COMPS 23Part23 SHMCOLOR COMPS 23 7 material type # 3 (Kinematic/Isotropic elastic-plastic) 23 23 23 0 ‘PART $HMNAME COMPS 24Part24 SHMCOLOR COMPS 24 8 material type # l (elastic) 24 24 24 0 *PART $HMNAME COMPS 25Part25 SHMCOLOR COMPS 25 9 material type # 3 (Kinematic/Isotropic elastic-plastic) 25 25 25 0 ‘PART $HMNAME COMPS 26Part26 $HMCOLOR COMPS 26 10 material type # l (rigid) 26 26 16 0 ‘PART $HMNAME COMPS lOlBARl $HMCOLOR COMPS 101 15 barl 101 101 101 ‘PART SHMNAME COMPS lOZBARZ SHMCOLOR COMPS 102 15 bar2 102 101 101 194 *PART $HMNAME COMPS $HMCOLOR COMPS bar3 103 101 ‘PART $HMNAME COMPS SHMCOLOR COMPS bar4 104 101 *PART $HMNAME COMPS SHMCOLOR COMPS Barrier end surface 105 102 *PART SHMNAME COMPS SHMCOLOR COMPS Barrier side surface 106 102 *PART SHMNAME COMPS $HMCOLOR COMPS Concrete barrier 107 103 *PART $HMNAME COMPS $HMCOLOR COMPS board 108 103 *PART SHMNAME COMPS $HMCOLOR COMPS 1 10 l 02 *PART SHMNAME COMPS $HMCOLOR COMPS 112 102 *SECTION_BEAM 103BAR3 103 15 101 1043AR4 104 15 101 IOSSURF_CROSS 105 1 102 106SIDESURF 106 9 102 107CONCRETE 107 l 103 108board 108 14 108 l lOcontath 1 10 4 102 1 12contact1 1 12 5 102 195 $HMNAME PROPS 18SectBeaml 8 18 l 0.0 2.0 75.0 75.0 71.0 71.0 *SECTION_SHELL $HMNAME PROPS ZSectSh112 2 2 0.0 3 l .0 1.0 1.0 1 .0 *SECTION_SOLID $HMNAME PROPS lSectSldl l l 4 *INITIAL_VELOCITY $HMNAME LOADCOLS lVelocity SHMCOLOR LOADCOLS l 1 7 0 13.4 0.0 0.0 0.0 $8 Base Accelerations and Angular Velocities *LOAD_BODY_Z SHMNAME LOADCOLS 3LoadBody_3 $HMCOLOR LOADCOLS 3 1 1 0.0 0 *ELEMENT_BEAM 43317 18 1 8 7 43318 18 8 9 7 ’ELEMENT_SHELL_THICKNESS 9 2 108 1 1 1 123 1.54 l .54 *SET_PART_LIST $HMSET SHMNAME SETS lset_part l l 2 3 4 9 10 l l 12 17 18 19 20 25 *SET_PART_LIST $HMSET 196 O. 1.0 0.0 0 121 1.54 13 21 0.0 0.0 0.0 0.0 1.54 14 22 0 0 0 7 8 15 16 23 24 $HMNAME SETS 28et_part.l 11 19 6Set_6 4304 4371 4450 4493 4572 4642 4682 4743 12 20 4330 4373 4452 4510 4574 4644 4699 4745 6setSegment_6 6 6 l 3car_tube 13 l 2 1 2 9 10 17 18 25 *SET_NODE_L1ST $HMS6T $HMNAM6 SETS 6 4300 4302 4355 4369 4422 4424 4489 4491 4544 4570 4623 4625 4678 4680 4724 4741 *SET_SEGMENT $HMNAM6 CSURFS SHMCOLOR CSURFS 6 ‘CONTACT_NODES_TO_SURFACE rurwntA866<3RLNJPS SHMCOLOR GROUPS 10 13 21 4332 4390 4454 45 12 4646 470 l *CONTACT_AUTOMATIC_SINGLE_SURFACE_TITLE $664304146<3anrps SHMCOLOR GROUPS 5singlesurface 2 0.15 0. 1.0 *RIGIDWALL_PLANAR 031 1.0 $HMNAME GROUPS $HMCOLOR GROUPS 6 452.93851-567.67354 *BOUNDARY_SPC_NODE SHMNAME LOADCOLS 5singlesurface 5 2 2 0.0 0.0 6rigid 6 12 0.0 1.0 -l .0 452.93851-567.67354 2NodalConstraints. 1 14 22 43 34 4392 447 l 45 14 4602 4660 4703 1.0 0.0 1.0 7 8 15 16 23 24 435 1 4353 4394 4420 4473 4475 4540 4542 4604 462 1 4662 4664 4720 4722 0.01 .0000E+20 1.0 SHMCOLOR LOADCOLS 2 5 5297 0 1 l 1 *DATABASE_HISTORY_NODE SHMNAME OUTPUTBLOCKS 1nodeth 2788110 2788108 2787921 2787919 *DEFINE_CURVE SHMNANIE CURVES lLoadCurvel $HMCOLOR CURVES l l $HMCURVE l l LoadCurvel l 0 1.0 1.0 0.0 0.0 0.0 3.0 0.00981 400.0 0.00981 $5 UNSUPPORTED CARDS - STARTS *MAT_PSEUDO_TENSOR 103 2.4E-06 8.971 0.2 0.02 -1.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 $5 UNSUPPORTED CARDS - ENDS I"END 198 0.0 0.0 0.0 APPENDIX B A STEEL BALL IMPACTING ON WOOD-CEMENT PARTICLEBOARD OVERLAYING A CONCRETE BLOCK This appendix presents the input file of a steel ball impacting a wood-cement particleboard overlaying a concrete block. For simplification, the original 477 pages input file was simplified into the current demonstration file. The current file only presents the major command syntax but eliminating most of the data related to Nodes and Elements. The input file is in keyword format in LS-DYNA Version 960 and generated using HyperMesh Version 5.1 and Text Editor as well. *KEYWORD $$ HM_OUTPUT_DECK created 02:33:56 05-26-2003 by HyperMesh Version 5.1 $$ Generated using HyperMesh—Ls-dyna Template Version : 5. l *CONTROL_TERMINATION $8 ENDTIM ENDCYC DTMIN ENDENG ENDMAS 10.0 0 0.0 0.0 0.0 *CONTROL_TIMESTEP $$ DTINIT TSSFAC ISDO TSLIMT DTZMS LCTM ERODE MSIST 0.00.89999998 0 0.0 0.0 0 l 0 *CONTROL_SHELL $8 WRPANG ITRIST IRNXX ISTUPD THEORY BWC MITER PROJ 45.0 2 -1 0 2 2 1 0 *CONTROL_HOURGLASS $$ IHQ QH 5 O. 1 *CONTROL_BULK_VISCOSITY $$ Q2 Q1 1 .5 0.06 *CONTROL_CONTACT $$ SLSFAC RWPNAL ISLCHK SHLTHK PENOPT THKCHG ORIEN ENMASS 0. 1 0.0 2 0 1 0 1 $5 USRSTR USRFRC NSBCS INTERM XPENE SSTHK ECDT TIEDPRJ 199 0 0 0 0 0.0 *CONTROL_PARALLEL $$ NCPU NUMRHS ACCU 4 0 1 *CONTROL_COUPLING $$ UNLENG UNTIME UNFORC TIMIDL SUBCYL 1.0 1.0 0.0 0.0 0 *CONTROL_OUTPUT $$ NPOPT NEECHO NREFUP IACCOP l 3 0 0 0.0 *CONTROL_ENERGY $3 HGEN RWEN SLNTEN RYLEN 2 2 2 2 $$DATABASE_OPTION - Control Cards for ASCII output *DATABASE_NODOUT 0.02 *DATABASE_GLSTAT 0.02 *DATABASE_MATSUM 0.02 ‘DATABASE_RBDOUT 0.02 l"DATABASE”BlNARYmD3PLOT $$ DT/CYCL LCDT BEAM NPLTC 1.0 0 0 0 ‘DATABASE_BINARY_D3THDT $$ DT/CYCL LCID 2.0 0 I"DATABASE_BINARY_D3DUMP $$ DT/CYCL 40000.0 I"DATABASE_BINARY__RUNRSF $$ DT/CYCL 10000.0 *NODE F LIPX OPIFS 23.2759301877E-15 -53.5 -0.503 *MAT_PLASTIC_KINEMATIC $11MNAM6 MATS lsphere 17.9000606 210.0 0.28 0.351 200 3.4 FLIPY IPNINT 100 0.0 FLIPZ IKEDIT 0 0.0 0.0 0.0 *MAT_NULL SHNINAME MATS 3Null 38.4000E-07 *MAT_PIECEWISE_LINEAR_PLASTICITY $HMNAME MATS 2board 21 .0400E-06 0.37 0.3 0.017 1 0 $$ HM Entries in Stress-Strain Curve = 0 *PART $HMNAME COMPS lsphere $HMCOLOR COMPS 1 4 l l 1 *PART $HMNAME COMPS 2board $HMCOLOR COMPS 2 2 2 2 2 *PART $HMNAME COMPS 3concrete $HMCOLOR CONIPS 3 8 3 3 4 ‘PART $HMNAME COMPS 4sphere_face $HMCOLOR COMPS 4 9 4 4 3 *PART $HMNAME COMPS 5board_face $HMCOLOR COMPS 5 7 5 5 3 *SECTION_SHELL $HMNAME PROPS 4sphere_face 4 2 0.833 2 0.0 0.0 0.1 0.1 0.1 0.1 0.0 $HMNAME PROPS 5board_face 201 200.0 0.3 5 2 0.833 2 0.0 0.0 0 0.1 0.1 0.1 0.1 0.0 *SECTION_SOLID $HMNAME PROPS lsphere 1 1 4 $HMNAME PROPS 2board 2 l 4 $HMNAME PROPS 3concrete 3 l 4 *ELEMENT_SHELL l 1586 4 2375 2373 2374 2374 l 1585 4 2222 2262 2263 2263 11584 4 2254 2221 2255 2255 11583 4 2095 2092 2118 2118 *ELEMENT_SHELL l 1978 4 2288 2306 2295 2278 1 1977 4 2282 2275 2294 2297 *ELEMENT_SOLID 1420 1 1359 165 172 207 207 207 207 207 1476 l 1401 356 315 357 357 357 357 357 *CONTACT_AUTOMATIC_SURFACE_TO_SURFACE $HMNAME GROUPS lsurftosurf $HMCOLOR GROUPS 1 l 4 5 3 3 0 0 0.0 0.0 0.0 0.0 0.0 0 0.01.0000E+20 1.0 1.0 1.0 1.0 1.0 1.0 *BOUNDARY_SPC_NODE $HMNAME LOADCOLS lspc $HMCOLOR LOADCOLS 1 14 8462 0 l l l 1 1 l *INITIAL_VELOC1TY_NODE $HMNAME LOADCOLS 2velocity $HMCOLOR LOADCOLS 2 10 2699 0.0 0.0 -l .72 2698 0.0 0.0 -1.72 I"DATABASE_HISTORY_NODE $HMNAME OUTPUTBLOCKS lNOUT 399 558 2295 202 *DEFINE_CURVE $HMNAME CURVES lcurvel $HMCOLOR CURVES l l $HMCURVE l 0 curvel l 0 1.0 1.0 0.0 0.0 0.0 0.0034 0.0102 0.0067 0.0206 0.0095 $$ UNSUPPORTED CARDS - STARTS *MAT_PSEUDO_TENSOR 4 2.4E-06 8.971 0.2 0.02 -l .0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 $$ UNSUPPORTED CARDS - ENDS *END 203 0.0 BIBLIOGRAPHY 204 BIBLIOGRAPH Altair Engineering Inc. 1999. 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