Resumen

Thermomechanical analysis of ablative materials is of great importance to the design of thermal-protection systems. A finite volume method for coupling the mechanical and thermal response models for ablation problems is proposed. This method is capable of simulating both transient and static thermomechanical responses. The solver is verified against analytic solutions and through code-to-code comparisons. It is then fully coupled to a state-of-the-art material response code. Coupled results show that high temperature gradients have significant effects on the mechanical performance and stress generation. The magnitude and the location ofthe stress concentration can play a significant role in structural integrity, and may lead to crack formation as well as spallation.

Idioma originalEnglish
Páginas (desde-hasta)369-379
Número de páginas11
PublicaciónJournal of Thermophysics and Heat Transfer
Volumen32
N.º2
DOI
EstadoPublished - 2018

Nota bibliográfica

Publisher Copyright:
© Copyright 2017 by Rui Fu, Haoyue Weng, Jonathan F. Wenk, and Alexandre Martin.

Financiación

Support for this work was provided by Kentucky EPSCoR and NASA award NNX13AN04A, and NASA award NNX16AD06A. The authors are grateful to E. Sozer at NASA Ames Research Center for insightful discussions on the modeling code.

FinanciadoresNúmero del financiador
Kentucky Statewide EPSCoR
National Aeronautics and Space Administration
National Aeronautics and Space AdministrationNNX13AN04A, NNX16AD06A

    ASJC Scopus subject areas

    • Condensed Matter Physics
    • Aerospace Engineering
    • Mechanical Engineering
    • Fluid Flow and Transfer Processes
    • Space and Planetary Science

    Huella

    Profundice en los temas de investigación de 'Thermomechanical coupling for charring ablators'. En conjunto forman una huella única.

    Citar esto