Determination of wall boundary conditions for high-speed-ratio direct simulation Monte Carlo calculations
Author:
Affiliation:
1. University of Tennessee Space Institute, Tullahoma, Tennessee 37388-8897
2. REMTECH, Inc., Huntsville, Alabama 35805
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26545
Reference23 articles.
1. Aerothermodynamics of a 1.6-meter-diameter sphere in hypersonic rarefied flow
2. 5Brewer, E. B. "Hypersonic Rarefied Wake Characterization," NASA TP 3327,1993.
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