Abstract
The KATS-US solver uses a modified Volume Averaged Navier-Stokes set of equations to model the interaction between ablative material and hypersonic flow. The approach uses a single set of equations for both fluid and porous domains. In the present work, a two-temperature model is added to the code. The implementation of the model was verified by comparing to published results. The thermal non-equilibrium effect within the porous medium is presented and discussed. A new equation is proposed that can be used to model vibrational accommodation inside the porous medium.
Original language | English |
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Title of host publication | AIAA SciTech Forum and Exposition, 2024 |
DOIs | |
State | Published - 2024 |
Event | AIAA SciTech Forum and Exposition, 2024 - Orlando, United States Duration: Jan 8 2024 → Jan 12 2024 |
Publication series
Name | AIAA SciTech Forum and Exposition, 2024 |
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Conference
Conference | AIAA SciTech Forum and Exposition, 2024 |
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Country/Territory | United States |
City | Orlando |
Period | 1/8/24 → 1/12/24 |
Bibliographical note
Publisher Copyright:© 2024 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
ASJC Scopus subject areas
- Aerospace Engineering