AWG ERIF Test Case 12: Single Rotating Fan Blade
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| Description: | Comparison of results from different cpu architectures for a single rotating fan blade. The model demonstrates a stable solution for the rotation of a blade. Specifically, the blade internal and kinetic energy should remain constant as the blade is rotated. An implicit analysis is required first to apply the rotational centrifugal load or preload to the blade. This analysis is followed by an explicit rotation of the blade where the stability of the blade internal and kinetic energies are evaluated. The implicit and explicit analysis are completed in one-step analysis by using the keyword input *CONTROL DYNAMIC RELAXATION with IDRFLAG=5. |
| Sub Test Case 1 uses a solid element discretization for the fan blade. | |
| Sub Test Case 2 uses a shell element discretization for the fan blade. | |
| Sub Test Case 3 uses a thick shell element discretization for the fan blade. | |
| Status: | Accepted and currently part of the AWG Test Suite |
| Classification: | Example |
| Input Deck: | Test Case 12 Input |
| Input Deck 07/11/2016 Update: | Added additional test cases using shell and thick shell discretizations of the fan blade. |
| Keywords: | *CONTROL_DYNAMIC_RELAXATION |
| *CONTROL_ACCURACY | |
| ... | |
| Units: | in (length), s (time), lbf-s2/in (mass), psi (stress), lbf-in (energy) |
| Model Data: | Sub Test Case ID 1: 4234 Nodes, 4104 solid elements |
| Sub Test Case ID 2: 1647 Nodes, 1560 shell elements | |
| Sub Test Case ID 3: 3294 Nodes, 1560 thick shell elements | |
| Run Time: | Sub Test Case ID 1: approx. total CPU time 6 min. 52 sec. (Intel® Xeon® CPU E7- 8837 @ 2.67GHz / MPP / 4 cpu's) |
| Sub Test Case ID 2: approx. total CPU time < 1 min. (Intel® Xeon® CPU E7- 8837 @ 2.67GHz / MPP / 4 cpu's) | |
| Sub Test Case ID 3: approx. total CPU time 1 min. 17 sec.(Intel® Xeon® CPU E7- 8837 @ 2.67GHz / MPP / 4 cpu's) | |
| Earliest Version : | LS-DYNA® R9.0 |
| Test Case Details and Results: | Test Case 12, Documentation and Results for LS-DYNA R14.1-7-gea5f83301c |
| Test Case 12, Documentation and Results for LS-DYNA R12.2 Revision 1-g2dd504fe3d | |
| Test Case 12, Documentation and Results for LS-DYNA R14.0 Revision 461-gee93a457ac | |
| Test Case 12, Documentation and Results for LS-DYNA R13.1 Revision 93-g6e31b592d7 | |
| Test Case 12, Documentation and Results for LS-DYNA R13.0 Revision 365-gf8a97bda2a | |
| Test Case 12, Documentation and Results for LS-DYNA R12.1 Revision 128-g57c3366e82 | |
| Test Case 12, Documentation and Results for LS-DYNA R12.0 Revision 1908-g604b5c7 | |
| Test Case 12, Documentation and Results for LS-DYNA R11.2 Revision 51-g7e1aee4 | |
| Test Case 12, Documentation and Results for LS-DYNA R11.1 Revision 139325 | |
| Test Case 12, Documentation and Results for LS-DYNA R10.2 Revision 134743 | |
| Test Case 12, Documentation and Results for LS-DYNA R11.0 Revision 130010 | |
| Test Case 12, Documentation and Results for LS-DYNA R9.3 Revision 126955 | |
| Test Case 12, Documentation and Results for LS-DYNA R10.1 Revision 123136 | |
| Test Case 12, Documentation and Results for LS-DYNA R9.2 Revision 118235 | |
| Test Case 12, Documentation and Results for LS-DYNA R10.0 Revision 116539 | |
| Test Case 12, Documentation and Results for LS-DYNA R9.1 Revision 113467 | |
| Test Case 12, Documentation and Results for LS-DYNA R9.0 Revision 108899 | |
| Bug Issues Found and Fixed: | Bug 16608: Incorrect MATSUM internal energy (shell and thick shell elements) in implicit-explicit switching model was fixed in 149106.trunk and 149107.R12 |
| Bug 10826: Error termination, single fan blade model (thick shell elements) | |
Test Case 12 History: Original Input Deck
| Input Deck: | Test Case 12 |
| Test Case Details and Results: | Test Case 12, Documentation and Results for LS-DYNA R8.0.0 Revision 96167 |
| Test Case 12, Documentation and Results for LS-DYNA R7.1.0 Revision 87770 | |
| Bug Issues Found and Fixed: | None |
last modified on Monday April 24, 2023 13:57:10 PDT