AWG ERIF Test Case 4: Steel Projectile Impacts Kevlar Fabric
| Image: | | |
| Animation: | Test Case 4 Animation | |
| Description: | Kevlar is a ballistic fabric with exceptionally high resistance to perforation. Due to its lightweight and mechanical properties is ideal to be used as containment material in jet engines. Often several layers of fabric are used to offer adequate protection to perforation from projectiles. The material model developed by Arizona State University (ASU) has the capability of modeling multiple layers of Kevlar fabric using multiple fabric plies in a single shell element. The advantage of this approach is reduced computational time (fewer element and contact calculations). | |
| Status: | Accepted and currently part of the AWG Test Suite | |
| Classification: | Validation | |
| Reference Reports: | Explicit Finite Element Modeling of Multilayer Composite Fabric for Gas Turbine Engine Containment Systems | |
| Fabric Material Tests and Modeling | ||
| Ballistic Impact Testing | ||
| Material Model Development | ||
| ASU Material Modeling and Numerical Simulations | ||
| ASU Material Fabric Material Tests | ||
| ASU Final Report | ||
| Input Deck: | Test Case 4 Input | |
| Input Deck 12/13/2018 Update: | Resolved Bug 14293 with contact input changes that include SOFT=2, SBOPT=3, DEPTH=23, and removing the initial penetration of the projectile using *DEFINE_TRANSFORMATION with an x-translation. | |
| Keywords: | *MAT_DRY_FABRIC (ASU material model Version 1.3) | |
| ... | ||
| Units: | in (length), ms (time), Mlbf-ms2/in (mass), Mlbf (force), Mpsi (stress), Mlbf-in (energy) | |
| Model Data: | CMS_LG612.in: | 40520 shells / 4 shell materials, 81652 solids / 3 solid materials, 7 parts |
| CMS_LG969.in: | 162240 shells / 16 shell materials, 28442 solids / 3 solid materials, 19 parts | |
| SMS_LG612.in: | 40320 shells / 4 shell materials, 28648 solids / 3 solid materials, 7 parts | |
| SMS_LG969.in: | 162280 shells / 16 shell materials, 28652 solids / 3 solid materials, 19 parts | |
| Run Time: | CMS_LG612.in: | approx. total CPU time = 23 minutes 19 seconds (Intel® Xeon® CPU E7- 8837 @ 2.67GHz / MPP / 4 cpu's) |
| CMS_LG969.in: | approx. total CPU time = 2 hours 27 minutes 54 seconds (Intel® Xeon® CPU E7- 8837 @ 2.67GHz / MPP / 4 cpu's) | |
| SMS_LG612.in: | approx. total CPU time = 8 minutes 9 seconds (Intel® Xeon® CPU E7- 8837 @ 2.67GHz / MPP / 4 cpu's) | |
| SMS_LG969.in: | approx. total CPU time = 1 hours 17 minutes 23 seconds (Intel® Xeon® CPU E7- 8837 @ 2.67GHz / MPP / 4 cpu's) | |
| Earliest Version : | LS-DYNA® R6.0.0 | |
| Test Case Details and Results: | Test Case 4, Documentation and Results for LS-DYNA R14.1-7-gea5f83301c | |
| Test Case 4, Documentation and Results for LS-DYNA R12.2 Revision 1-g2dd504fe3d | ||
| Test Case 4, Documentation and Results for LS-DYNA R14.0 Revision 461-gee93a457ac | ||
| Test Case 4, Documentation and Results for LS-DYNA R13.1 Revision 93-g6e31b592d7 | ||
| Test Case 4, Documentation and Results for LS-DYNA R13.0 Revision 365-gf8a97bda2a | ||
| Test Case 4, Documentation and Results for LS-DYNA R12.1 Revision 128-g57c3366e82 | ||
| Test Case 4, Documentation and Results for LS-DYNA R12.0 Revision 148708 | ||
| Test Case 4, Documentation and Results for LS-DYNA R11.2 Revision 51-g7e1aee4 | ||
| Test Case 4, Documentation and Results for LS-DYNA R11.1 Revision 139325 | ||
| Test Case 4, Documentation and Results for LS-DYNA R10.2 Revision 134743 | ||
| Test Case 4, Documentation and Results for LS-DYNA R11.0 Revision 130010 | ||
| Bug Issues Found and Fixed: | None | |
Test Case 4 History: 02/12/2014 Update
| Input Deck: | Test Case 4 | |
| Input Deck Updates: | The user material model was replaced with *MAT_DRY_FABRIC, which is available in LS-DYNA R7.1 and later versions. | |
| Test Case Details and Results: | Test Case 4, Documentation and Results for LS-DYNA R9.3 Revision 126955 | |
| Test Case 4, Documentation and Results for LS-DYNA R10.1 Revision 123136 | ||
| Test Case 4, Documentation and Results for LS-DYNA R9.2 Revision 118235 | ||
| Test Case 4, Documentation and Results for LS-DYNA R10.0 Revision 116539 | ||
| Test Case 4, Documentation and Results for LS-DYNA R9.1 Revision 113467 | ||
| Test Case 4, Documentation and Results for LS-DYNA R9.0 Revision 108899 | ||
| Test Case 4, Documentation and Results for LS-DYNA R8.0.0 Revision 96167 | ||
| Test Case 4, Documentation and Results for LS-DYNA R7.1.0 Revision 87770 | ||
| Bug Issues Found and Fixed: | Bug 14293: Differences in mat_sum_kinetic_energy of projectile. | |
Test Case 4 History: 01/02/2012 Update
| Input Deck: | Test Case 4 | |
| Input Deck Updates: | The Zylon material model was replaced with a Kevlar material model because of the predominant use of Kevlar in the aerospace industry. | |
| Test Case Details and Results: | Test Case 4, Documentation and Results for LS-DYNA R7.0.0 Revision 79069 | |
| Test Case 4, Documentation and Results for LS-DYNA R6.1 Revision 74184 | ||
| Test Case 4, Documentation and Results for LS-DYNA R6.0.0 Revision 71381 | ||
| Bug Issues Found and Fixed: | None | |
Test Case 4 History: 01/07/2011 Original Input Deck
| Input Deck: | Test Case 4 | |
| Test Case Details and Results: | Test Case 4, Documentation and Results for LS-DYNA R5.1.1 Revision 67000 | |
| Test Case 4, Documentation and Results for LS-DYNA R5.1.1 Revision 67628 | ||
| Bug Issues Found and Fixed: | None | |
last modified on Monday April 24, 2023 13:43:36 PDT