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AWG ERIF Test Case 5: Bird Strike on Rigid Plate
Image: QA_test_example_5__Bird_Strike_on_Rigid_Plate__model_image_web
Animation: Test Case 5 Animation
Description: A bird strike on a rigid plate (as replacement for a composite inlet of jet engine) is modeled with Lagrangian, ALE, SPH, S-ALE, and S-ALE with trimming approaches for the bird. This input deck serves as an example to provide consistent results among platforms and versions of the code as well as between the different modeling approaches.
Status: Accepted and currently part of the AWG Test Suite
Classification: Example
Input Deck: Test Case 5 Input
Input Deck 03/14/2018 Update: Structured ALE (S-ALE) and S-ALE with trimming models for the bird added.
Keywords: *MAT_NULL
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Units: in (length), s (time), lbf-s2/in (mass), psi (stress), lbf-in (energy)
Model Data: Lagrangian approach: 14400 shells / 1 shell material, 432 solids / 1 solid material, 2 parts
ALE approach: 16230 shells / 2 shell material, 84800 solids / 1 solid material, 3 parts
SPH approach: 14400 shells / 1 shell material, 15912 SPH nodes / 1 SPH material, 2 parts
Run Time: Lagrangian approach: approx. total CPU time = 1 minutes 33 seconds (Intel® Xeon® CPU E7- 8837 @ 2.67GHz / MPP / 4 cpu's)
ALE approach: approx. total CPU time = 7 minutes 12 seconds(Intel® Xeon® CPU E7- 8837 @ 2.67GHz / MPP / 4 cpu's)
SPH approach: approx. total CPU time = 13 minutes 36 seconds (Intel® Xeon® CPU E7- 8837 @ 2.67GHz / MPP / 4 cpu's)
Earliest Version: LS-DYNA® R4.2.1
Test Case Details and Results: Test Case 5, Documentation and Results for LS-DYNA R14.1-7-gea5f83301c
Test Case 5, Documentation and Results for LS-DYNA R12.2 Revision 1-g2dd504fe3d
Test Case 5, Documentation and Results for LS-DYNA R14.0 Revision 461-gee93a457ac
Test Case 5, Documentation and Results for LS-DYNA R13.1 Revision 93-g6e31b592d7
Test Case 5, Documentation and Results for LS-DYNA R13.0 Revision 365-gf8a97bda2a
Test Case 5, Documentation and Results for LS-DYNA R12.1 Revision 204-g810450fa20
Test Case 5, Documentation and Results for LS-DYNA R12.0 Revision 148708
Test Case 5, Documentation and Results for LS-DYNA R11.2 Revision 51-g7e1aee4
Test Case 5, Documentation and Results for LS-DYNA R11.1 Revision 139325
Test Case 5, Documentation and Results for LS-DYNA R11.0 Revision 130010
Bug Issues Found and Fixed: BUG 18081 in subcases 5.4 and 5.5: Error in subroutine wtalecps and changes to matsum internal energy. The error affected releases R12.1, R13.0, and R13.1 and the fixes are in R12.1 and R13.1, but not R13.0

Test Case 5 History: 03/14/2018 Update

Test Case 5 History: 02/09/2012 Update
Input Deck: Test Case 5
Input Deck Updates: Modifications were made to the ALE input deck. The usage of *INITIAL_VOLUME_FRACTION_GEOMETRY in this test case was incorrect. There is only one ALE multi-material group in the model, but in the *INITIAL_VOLUME_FRACTION_GEOMETRY card, it specifies changing the material inside a shell from AMMG 2 to AMMG 1. It passed the previous test, but failed with a newly added check to make sure the change from and to AMMG IDs are in the correct range.
Test Case Details and Results: Test Case 5, Documentation and Results for LS-DYNA R7.0.0 Revision 79069
Test Case 5, Documentation and Results for LS-DYNA R6.1 Revision 74159
Test Case 5, Documentation and Results for LS-DYNA R6 Revision 71731
Bug Issues Found and Fixed: BUG 6831 Different internal energy for SMP and MPP (ALE), Keyword: *DATABASE_MATSUM, fixed in R6.71666 and dev.71665

Test Case 5 History: 07/27/2011 Original Input Deck
Input Deck: Test Case 5
Test Case Details and Results: Test Case 5, Documentation and Results for LS-DYNA R5.1.1 Revision 67628
Bug Issues Found and Fixed: None



last modified on Monday April 24, 2023 13:49:20 PDT