TY - GEN
T1 - Multi-Fidelity Modeling Framework for Radiative Transfer in Hypersonic Atmospheric Entry
AU - Jo, Sung Min
AU - Kumar, Sanjeev
AU - Maout, Vincent Le
AU - Munafò, Alessandro
AU - Panesi, Marco
N1 - Publisher Copyright:
© 2023, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2023
Y1 - 2023
N2 - This work aims to construct a multi-fidelity modeling framework for radiative transfer in hypersonic environment and its applications. Analyses of the radiation phenomena in such extreme conditions require covering a wide range of physical aspects, including coupling with other physics, such as high-enthalpy flows and electromagnetism, for completeness of the investigation. This requirement has been achieved by constructing a numerical toolbox, MURP (MUlti-fidelity Radiation Package), through the present work. The proposed framework offers non-gray and non-equilibrium gaseous radiative transport analysis capability with various levels of fidelity ranging from a one-dimensional tangent-slab method to multi-dimensional finitevolume treatments, while the spectral properties, such as absorption and emission coefficients of gas mixtures, are calculated by either a line-by-line method or reduced-order spectral models. The developed framework is then applied to hypersonic atmospheric entry cases, including the FIRE II and Dragonfly flight missions and the ground testing facility of an inductively coupled plasma torch. The applications reveal the impact of the radiation coupling while validating the framework’s accuracy by reproducing reference data.
AB - This work aims to construct a multi-fidelity modeling framework for radiative transfer in hypersonic environment and its applications. Analyses of the radiation phenomena in such extreme conditions require covering a wide range of physical aspects, including coupling with other physics, such as high-enthalpy flows and electromagnetism, for completeness of the investigation. This requirement has been achieved by constructing a numerical toolbox, MURP (MUlti-fidelity Radiation Package), through the present work. The proposed framework offers non-gray and non-equilibrium gaseous radiative transport analysis capability with various levels of fidelity ranging from a one-dimensional tangent-slab method to multi-dimensional finitevolume treatments, while the spectral properties, such as absorption and emission coefficients of gas mixtures, are calculated by either a line-by-line method or reduced-order spectral models. The developed framework is then applied to hypersonic atmospheric entry cases, including the FIRE II and Dragonfly flight missions and the ground testing facility of an inductively coupled plasma torch. The applications reveal the impact of the radiation coupling while validating the framework’s accuracy by reproducing reference data.
UR - http://www.scopus.com/inward/record.url?scp=85197745311&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85197745311&partnerID=8YFLogxK
U2 - 10.2514/6.2023-1730
DO - 10.2514/6.2023-1730
M3 - Conference contribution
AN - SCOPUS:85197745311
SN - 9781624106996
T3 - AIAA SciTech Forum and Exposition, 2023
BT - AIAA SciTech Forum and Exposition, 2023
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA SciTech Forum and Exposition, 2023
Y2 - 23 January 2023 through 27 January 2023
ER -