The NASA Ames Aerothermodynamics Branch provides NASA with integrated modeling, simulation, and test capabilities in the areas of aerothermodynamics, shock layer radiation, and entry system design. Our core capabilities include CFD simulation for entry vehicles at hypersonic velocities, including arc jet facility flow modeling and characterization; modeling and testing of shock layer kinetics and radiation; development of flow-field diagnostic techniques; and aero- and aerothermal testing via ballistic ranges. This presentation provides a brief technical introduction to the branches work and our capabilities in these areas.
The NASA Ames Aerothermodynamics Branch (Code TSA)
HyCUBE Technical Exchange Meeting ; 2020 ; Mountain View, CA, US
Sonstige
Keine Angabe
Englisch
NASA Ames Aerothermodynamics Branch (Code TSA)
NTIS | 2020
|NASA Ames Aerothermodynamics Branch
NTIS | 2022
|Aerothermodynamics research at NASA Ames
NTRS | 1987
|Aerothermodynamics Research at NASA AMES
NTIS | 1987
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