Abstract
Thermo-mechanical analysis of ablative materials is of great importance to Thermal Protection System design. A coupling method for thermo-mechanical and ablation response model is proposed using a Finite Volume approach. This method is capable of simulating both transient and static structural response. The solver is verified using a series of test cases and then fully coupled to a material response code. Coupled results show that the temperature field has a significant effect on mechanical performance and stress generation which can lead to mechanical fracture as well as spallation.
Original language | English |
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State | Published - Jun 13 2016 |
Event | 46th AIAA Thermophysics Conference, 2016 - Washington, United States Duration: Jun 13 2016 → Jun 17 2016 |
Conference
Conference | 46th AIAA Thermophysics Conference, 2016 |
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Country/Territory | United States |
City | Washington |
Period | 6/13/16 → 6/17/16 |
Bibliographical note
Publisher Copyright:© 2016 by Rui Fu, Haoyue Weng, Alexandre Martin and Jonathan F. Wenk. Published by the American Institute of Aeronautics and Astronautics, Inc.
ASJC Scopus subject areas
- Aerospace Engineering
- Mechanical Engineering