TY - GEN
T1 - In-depth Chemistry Model for High Temperature Oxidation of Carbon-based Thermal Protection System Materials
AU - Arias, Victoria
AU - Johnson, Harley T.
AU - Stephani, Kelly A.
N1 - Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc.. All rights reserved.
PY - 2022
Y1 - 2022
N2 - An in-depth surface chemistry model is proposed for high-temperature oxidation of carbon-based thermal protection system materials. This work builds upon a recently developed finite-rate oxidation model by incorporating additional subsurface processes at the microscale including subsurface oxygen transport and the oxidation reaction front as a function of material depth. The direct simulation Monte Carlo (DSMC) code, SPARTA, is used to simulate the interaction of high temperature atomic oxygen within layers of graphene. Reaction rates are determined from the ten-mechanism finite rate model of Gopalan et al., while subsurface transport of oxygen via advection is modeled using a novel multilayer oxidation model. This multilayer oxidation code captures the competition between oxygen transport and carbon removal at material wall temperatures in the extreme temperatures of atmospheric reentry conditions, allowing for quantification of both subsurface oxygen concentration profiles and the reaction front. We present in-depth oxygen concentration profiles, reaction front and recession rates for a 1D configuration, and we discuss the implications and importance of a 3D configuration.
AB - An in-depth surface chemistry model is proposed for high-temperature oxidation of carbon-based thermal protection system materials. This work builds upon a recently developed finite-rate oxidation model by incorporating additional subsurface processes at the microscale including subsurface oxygen transport and the oxidation reaction front as a function of material depth. The direct simulation Monte Carlo (DSMC) code, SPARTA, is used to simulate the interaction of high temperature atomic oxygen within layers of graphene. Reaction rates are determined from the ten-mechanism finite rate model of Gopalan et al., while subsurface transport of oxygen via advection is modeled using a novel multilayer oxidation model. This multilayer oxidation code captures the competition between oxygen transport and carbon removal at material wall temperatures in the extreme temperatures of atmospheric reentry conditions, allowing for quantification of both subsurface oxygen concentration profiles and the reaction front. We present in-depth oxygen concentration profiles, reaction front and recession rates for a 1D configuration, and we discuss the implications and importance of a 3D configuration.
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U2 - 10.2514/6.2022-1641
DO - 10.2514/6.2022-1641
M3 - Conference contribution
AN - SCOPUS:85123585956
SN - 9781624106316
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
BT - AIAA SciTech Forum 2022
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
Y2 - 3 January 2022 through 7 January 2022
ER -