Resumen
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.
| Idioma original | English |
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| Título de la publicación alojada | AIAA SciTech Forum and Exposition, 2024 |
| DOI | |
| Estado | Published - 2024 |
| Evento | AIAA SciTech Forum and Exposition, 2024 - Orlando, United States Duración: ene 8 2024 → ene 12 2024 |
Serie de la publicación
| Nombre | AIAA SciTech Forum and Exposition, 2024 |
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Conference
| Conference | AIAA SciTech Forum and Exposition, 2024 |
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| País/Territorio | United States |
| Ciudad | Orlando |
| Período | 1/8/24 → 1/12/24 |
Nota bibliográfica
Publisher Copyright:© 2024 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
ASJC Scopus subject areas
- Aerospace Engineering