Resumen
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.
| Idioma original | English |
|---|---|
| Estado | Published - jun 13 2016 |
| Evento | 46th AIAA Thermophysics Conference, 2016 - Washington, United States Duración: jun 13 2016 → jun 17 2016 |
Conference
| Conference | 46th AIAA Thermophysics Conference, 2016 |
|---|---|
| País/Territorio | United States |
| Ciudad | Washington |
| Período | 6/13/16 → 6/17/16 |
Nota bibliográfica
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
Huella
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