TY - GEN
T1 - Fully Coupled Material Response Solver using Radiative Transfer for Thermal Protection Systems
AU - Sirmalla, Prathamesh R.
AU - Chiodi, Robert
AU - Panesi, Marco
AU - Bodony, Daniel J.
N1 - Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2022
Y1 - 2022
N2 - This work presents an accurate model for the description of the radiative transfer processes that take place in reacting porous media subjected to high temperatures. In it, we solve the transport equation for radiation leveraging a low order spherical harmonic expansion, P1, to describe the angular dependence of the radiative intensity. This radiation model is tightly coupled with CHyPS, a material response solver developed within the CHESS that can simulate the heat and mass transfer in porous materials. CHyPS solves volume-averaged governing conservation equations for solid mass, gas mass, species (finite-rate chemistry), momentum, and energy. Model predictions are compared against several test cases published in literature demonstrating excellent agreement in the predictions. Finally, we present a demonstrative simulation of the heat shield used for the Dragonfly mission’s entry capsule.
AB - This work presents an accurate model for the description of the radiative transfer processes that take place in reacting porous media subjected to high temperatures. In it, we solve the transport equation for radiation leveraging a low order spherical harmonic expansion, P1, to describe the angular dependence of the radiative intensity. This radiation model is tightly coupled with CHyPS, a material response solver developed within the CHESS that can simulate the heat and mass transfer in porous materials. CHyPS solves volume-averaged governing conservation equations for solid mass, gas mass, species (finite-rate chemistry), momentum, and energy. Model predictions are compared against several test cases published in literature demonstrating excellent agreement in the predictions. Finally, we present a demonstrative simulation of the heat shield used for the Dragonfly mission’s entry capsule.
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U2 - 10.2514/6.2022-4005
DO - 10.2514/6.2022-4005
M3 - Conference contribution
AN - SCOPUS:85135377418
SN - 9781624106354
T3 - AIAA AVIATION 2022 Forum
BT - AIAA AVIATION 2022 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA AVIATION 2022 Forum
Y2 - 27 June 2022 through 1 July 2022
ER -