Computational Prediction of Aerothermodynamic Characteristics of a Reentry Vehicle at High Angles of Attack
Author:
Affiliation:
1. Air Force Research Laboratory
2. Andrews Space, Inc.
3. SAIC
4. U.S. Air Force Academy
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-2240
Reference16 articles.
1. 2AirForceResearchLaboratory,AirVehiclesDirectorate,January2006.
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1. Aeroheating study of Hypersonic Chemical Nonequilibrium Flows around a Reentry Blunt Body;AIAA SPACE 2014 Conference and Exposition;2014-08-01
2. Control of High-Angle-of-Attack Reentry Flow with Plasma Actuators;Journal of Spacecraft and Rockets;2013-03
3. Hypersonic Flow Computations for an Elliptic Cone at High Angle of Incidence;Journal of Spacecraft and Rockets;2012-05
4. Development of a Hypersonic Aerodynamic Database for a High Angle of Attack Reentry Configuration;17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2011-04-11
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