Resumen
Two-way coupling is performed between a spallation code and a hypersonic aerother- modyanmics CFD solver to evaluate the effect of spalled particles on the flow field. Time accurate solutions are computed in argon and air flow fields. A single particle simulations and multiple particles simulations are performed and studied.
| Idioma original | English |
|---|---|
| Estado | Published - ene 4 2016 |
| Evento | 54th AIAA Aerospace Sciences Meeting, 2016 - San Diego, United States Duración: ene 4 2016 → ene 8 2016 |
Conference
| Conference | 54th AIAA Aerospace Sciences Meeting, 2016 |
|---|---|
| País/Territorio | United States |
| Ciudad | San Diego |
| Período | 1/4/16 → 1/8/16 |
Nota bibliográfica
Funding Information:Financial support for this work was provided by NASA Kentucky EPSCoR Award NNX10AV39A, and NASA award NNX13AN04A.
Publisher Copyright:
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA . All rights reserved.
Financiación
Financial support for this work was provided by NASA Kentucky EPSCoR Award NNX10AV39A, and NASA award NNX13AN04A.
ASJC Scopus subject areas
- Aerospace Engineering
Huella
Profundice en los temas de investigación de 'Effects of spalled particles thermal degradation on a hypersonic flow field environment'. En conjunto forman una huella única.Citar esto
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