Development of a Hypersonic Aerodynamic Database for a High Angle of Attack Reentry Configuration
Author:
Affiliation:
1. Air Force Research Laboratory
2. SAIC
3. Valley Forge Scientific, LLC
4. Arnold Engineering Development Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-2239
Reference9 articles.
1. 1Brauer, G. L., Cornick, D. E. and Stevenson, R. "Capabilities and Appplications of the Program to Optimize Simulated Trajectories(POST),"NASACR-2770,Feb.1977.
2. 3Sponable,J.,Morse,A.,Raymer,D."MilitarySpacePlaneFlightDemonstrationConcepts,"AIAA-2004-4184,Jul.2004.
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Control of High-Angle-of-Attack Reentry Flow with Plasma Actuators;Journal of Spacecraft and Rockets;2013-03
2. Hypersonic Flow Computations for an Elliptic Cone at High Angle of Incidence;Journal of Spacecraft and Rockets;2012-05
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