cross section crash boxes

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Figure 7.20. Sequential deformation pictures of crash box with montage parts a)Empty, b) F1 foam filled and c) F2 foam filled (Geometry G2, t= 2.5 mm.) ................................................................................................... 151 Figure 7.21. Sequential deformation pictures of crash box with montage parts a) empty, b) F1 foam filled and c) F2 foam filled (Geometry G2, t= 2 mm) .......................................................................................................... 152 Figure 7.22. Load-displacement graphs of empty crash box with fixing parts a) 3 mm, b) 2.5 mm and c)2 mm thickness. .................................................... 154 Figure 7.23. Load-displacement graphs of F1 foam filled crash box with fixing parts a) 3 mm, b) 2.5 mm and c)2 mm thickness. .................................... 155 Figure 7.24. Load-displacement graphs of F2 foam filled crash box with fixing parts a) 3 mm, b) 2.5 mm and c)2 mm thickness. .................................... 156 Figure 7.25. Deformations pictures of empty and filled crash boxes in quasi- static and dynamic testing and simulation. ............................................... 157 Figure 7.26. Experimental and numerical load-displacement graphs of a) empty and b) partially filled crash box. ............................................................... 158 Figure 8.1. Load-displacement curves of empty and foam filled 1050H14 crush box, thicknesses of a) 1.5 mm and b) 3 mm. .................................. 160 Figure 8.2. The variation of (a) mean load and (a) SEA of 1050H14 crush boxes with foam relative density and box wall thickness. ....................... 161 Figure 8.3. Response surface foam filled 1050H14 crush box; a) mean load and b) SEA vs. foam relative density and box thickness. ............................... 162 Figure 8.4. Comparison between simulation and response surface analysis of a) mean load-foam relative density , b) SEA vs. foam relative density curves. ...................................................................................................... 163 Figure 8.5. Load-displacement curves of empty and partially Hydro foam-filled 6061T4 Al crush box with a wall thickness of 2 mm. .............................. 165 Figure 8.6. Response surface of mean load of filled boxes; a) Alulight and b) Hydro foam filling. ................................................................................... 166 Figure 8.7. Response surface of SEA of filled boxes; a) Alulight and b) Hydro foam filling. .............................................................................................. 167 Figure 8.8. Mean load and SEA vs. empty box thickness; a) 1050H14 and b) 6061T4 Al crash box. ............................................................................... 169 xviii
Figure 9.1. Pm,e vs. thickness graph for a) G1, b) G2, c) G1WP and d) G2WP empty crash boxes .................................................................................... 172 Figure 9.2. The change of Pm with filler relative density; a) G1, b) G2, c) G1WP and d) G2WP empty and partially foam filled crash boxes. ....... 173 Figure 9.3. a) 2D and b) 3D representation of Pm vs. thickness graphs for dynamic simulation of G1WP. ................................................................. 174 Figure 9.4. Stroke efficiency vs. relative density graphs of a) G1, b)G2, c) G1WP and d)G2WP. ................................................................................ 175 Figure 9.5. Stroke efficiency vs. plateau stress relative density change ratio. ........... 176 Figure 9.6. Crush force efficiency vs. relative density of a) G1, b)G2, c)G1WP and d)G2WP. ............................................................................................ 178 Figure 9.7. AE vs. plateau stress /relative density of crash boxes a) without and b)with fixing plate. ................................................................................... 179 Figure 9.8. Total efficiency vs. relative density of a) G1, b)G2, c)G1WP and d)G2WP. ................................................................................................... 181 Figure 9.9. The variation of strengthening coefficient with foam plateau stress relative density ratio in fully and partially filled boxes............................ 183 Figure 9.10. Energy-absorbing effectiveness factor for a) statically and b) dynamically tested boxes. ........................................................................ 186 Figure 9.11. SEA vs. relative density of a) G1, b)G2, c)G1WP and d)G2WP. ........... 188 Figure 9.12. 3D plot of SEA variation with thickness and filler relative density for G1WP crash box. ................................................................................ 189 xix
Page 1 and 2: OPTIMIZATION OF THE AXIAL CRUSHING
Page 3 and 4: ACKNOWLEDGEMENTS My PhD quest has b
Page 5 and 6: ÖZET KAPALI HÜCRELİ ALUMİNYUM K
Page 7 and 8: CHAPTER 4 EXPERIMENTAL DETAILS ....
Page 9 and 10: CHAPTER 8 ALUMINUM CRASH BOX OPTIMI
Page 12 and 13: Figure 3.7. Simulations of the defo
Page 14 and 15: Figure 4.9. Dimensions of tensile t
Page 16 and 17: Figure 6.21. Sequential deformation
Page 20 and 21: LIST OF TABLES Table Page Table 4.1
Page 22 and 23: Figure 1. 1. The body in white stru
Page 24 and 25: Figure 1. 4. Commercial crash boxes
Page 26 and 27: CHAPTER 2 AL CLOSED CELL FOAMS: PRO
Page 28 and 29: The processing methods and mechanic
Page 30 and 31: Figure 2. 5 The preferred particle
Page 32 and 33: Figure 2. 8. Typical cellular struc
Page 34 and 35: Figure 2. 10. Manufacturing cost of
Page 36: Figure 2. 12. Laser assisted foamed
Page 41 and 42: Figure 2.16. Shear strength, normal
Page 43 and 44: Figure 2. 19. Yield strength vs. re
Page 45 and 46: Figure 2. 21. Unit cell geometry an
Page 47 and 48: Figure 2. 24. Load-displacement cur
Page 49 and 50: Figure 2. 26. The photographs of a
Page 51 and 52: CHAPTER 3 CRUSHING BEHAVIOR OF TUBU
Page 53 and 54: Figure 3.2. Diamond deformation mod
Page 57 and 58: deformation mode transition from ax
Page 59 and 60: Figure 3.8. Energy absorption of qu
Page 61: (a) (c) Figure 3.10. Deformation mo
Page 65 and 66: (a) (b) Figure 3.13. a) Schematic o
Page 67 and 68: (a) (b) (c) Figure 3.15. a) Load-di
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Figure 3.18. The crush terminology.
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The quasi-static compression behavi
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Figure 3.22. The variation of speci
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Figure 3.24. Deformation modes of e
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Figure 3.27. SEA values of empty an
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Figure 3.29. (cont.) 3.5. Motivatio
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CHAPTER 4 EXPERIMENTAL DETAILS 4.1.
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(a) (b) Figure 4.3.Pictures of a) f
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oxes are shown in Figure 4.6. The l
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Figure 4.7. The method of trigger m
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4.4. Compression Tests of Crash Box
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4.5.2. Uniaxial Compression Testing
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Table 4.1 (Cont.) G1 T3 F2 G1T3F2 3
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Table 4.2 (Cont.) G1 T2.5 WP F2 G1T
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CHAPTER 5 SIMULATION AND OPTIMIZATI
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considered in axial and transverse
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were constrained. Since the width o
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5.4. The Crashworthiness Optimizati
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great effect on the crushing behavi
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CHAPTER 6 EXPERIMENTAL RESULTS 6.1.
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Figure 6.3.Tensile stress-strain cu
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(a) (b) Figure 6.5. Sequential defo
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plate (Figure 6(b)). The trigger is
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(a) (b) Figure 6.9. Deformation seq
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Figure 6.12. Sequential deformation
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Figure 6.18. (cont.) (c) (a) (b) Fi
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Figure 6.20.(cont.). (b) (c) 6.5.4.
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Figure 6.21.(cont.) (b) (c) 122
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Figure 6.22.(cont.) (c) Figure 6.23
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Figure 6.24.(Cont.) (b) (c) (a) Fig
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Figure 6.26.(cont.) (b) (c) 6.6. Dy
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Figure 6.27. (cont.) (b) (c) 130
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CHAPTER 7 MODELING RESULTS OF FOAM,
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experimental tensile stress-strain
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significant effect of weld seem ope
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Figure 7.7. Deformation photo of fi
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Figure 7.11. Deformation photos of
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(a) (b) (c) Figure 7.14. Load-displ
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7.4. Simulation of Empty and Partia
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Figure 7.16. (cont.) (c) (a) Figure
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(a) (b) Figure 7.18. Sequential def
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Figure 7.19. (cont.) (b) (c) 150
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Figure 7.20. (cont.) (c) (a) Figure
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(a) (b) Figure 7.26. Experimental a
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The constructed response surface of
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Table 8.1. R 2 , Radj 2 and RMSE va
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(a) (b) Figure 8.7. Response surfac
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an empty tube wall thickness higher
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where, K is a dimensionless constan
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The dynamic simulation and analytic
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Figure 9.4. (cont.) (c) (d) Figure
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Figure 9.6. (cont.) (c) (d) (a) Fig
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Equation 9.7 can also be rewritten
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(a) (b) Figure 9.10. Energy-absorbi
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Figure 9.11. (cont.) (d) The variat
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foam filling were evaluated. The re
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13. The interaction between foam fi
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Arora, J. S.,2004,Introduction to O
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Dannemann, K. A. and Lankford, J.,
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Hall, I. W., Guden, M. and Yu, C. J
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Kim, D-K. and Lee, S., 1999, Impact
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Mamalis, A. G., Manolakos, D. E., I
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Pugsley, A. G. and Macaulay, M., 19
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T. Miyoshi, M. Itoh S. Akiyama A. K
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Zhao, H., Elnasri, I. and Girard, Y
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