Development of a coupled thermo-mechanical solver for ablation problems

Rui Fu, Haoyue Weng, Jonathan F. Wenk, Alexandre Martin

Research output: Contribution to conferencePaperpeer-review

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 languageEnglish
StatePublished - Jun 13 2016
Event46th AIAA Thermophysics Conference, 2016 - Washington, United States
Duration: Jun 13 2016Jun 17 2016

Conference

Conference46th AIAA Thermophysics Conference, 2016
Country/TerritoryUnited States
CityWashington
Period6/13/166/17/16

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

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