Material Response Modelling of Ablating Thin Layers

H. Berk Gür, Rui Fu, Alexandre Martin

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

The state-of-the-art volume-averaging thin-layer approach is a highly advanced method capable of accurately predicting the material response when different materials are present. Extensive validation in previous studies has confirmed its reliability and accuracy. In the current analysis, complex geometries such as is o-q and flat-face cylinders have been specifically selected to examine the behavior of the thin layer. The thin layer material chosen for this investigation is room-temperature vulcanized rubber (RTV), which undergoes a phase change during the simulation. Initially, the RTV is impermeable, effectively blocking the passage of pyrolysis gases and heat. However, as the RTV transforms into char, it undergoes a change in its permeability, allowing the flow to pass through it. This dynamic behavior of the RTV, including the permeability transition, is effectively captured in the analyses, enhancing the overall understanding of the system.

Original languageEnglish
Title of host publicationAIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023
DOIs
StatePublished - 2023
EventAIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023 - San Diego, United States
Duration: Jun 12 2023Jun 16 2023

Publication series

NameAIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023

Conference

ConferenceAIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023
Country/TerritoryUnited States
CitySan Diego
Period6/12/236/16/23

Bibliographical note

Publisher Copyright:
© 2023, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.

Funding

Funding for this work was provided in part by NASA ACCESS STRI award No. 80NSSC21K1117. The analyses were completed using The Lipscomb Compute Cluster(LCC). The first author would like to thank K. Price for reviewing the manuscript.

FundersFunder number
NASA80NSSC21K1117

    ASJC Scopus subject areas

    • Energy Engineering and Power Technology
    • Nuclear Energy and Engineering
    • Aerospace Engineering

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