Hypersonic rarefied flow past spheres including wake structure
Author:
Affiliation:
1. ViGYAN, Inc., Hampton, Virginia 23666-0325
2. NASA Langley Research Center, Hampton, Virginia 23681-0001
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Reference19 articles.
1. Direct simulation of aerothermal loads for an aeroassist flight experiment vehicle
2. Three-dimensional rarefied flow simulations for the Aeroassist Flight Experiment vehicle
3. Three dimensional discrete particle simulation of an AOTV
4. Computation of near-wake, aerobrake flowfields
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