Abstract
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.
Original language | English |
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State | Published - Jan 4 2016 |
Event | 54th AIAA Aerospace Sciences Meeting, 2016 - San Diego, United States Duration: Jan 4 2016 → Jan 8 2016 |
Conference
Conference | 54th AIAA Aerospace Sciences Meeting, 2016 |
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Country/Territory | United States |
City | San Diego |
Period | 1/4/16 → 1/8/16 |
Bibliographical note
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.
ASJC Scopus subject areas
- Aerospace Engineering