Comparison of High Angle of Attack Computational and Experimental Aerothermal Data for a Reusable Reentry Vehicle

Author:

Tejtel Daniel1,Wadhams Timothy2,Klaput Robert3,Vernot Rebecca3,Hudson Douglas3,Rajendran Natesan3

Affiliation:

1. Air Force Research Laboratory

2. CUBRC

3. SAIC

Publisher

American Institute of Aeronautics and Astronautics

Reference9 articles.

1. 5Rothnie, M. D., and Acheson, K. A. "Fast and Accurate Use of Unstructured CFD Methods to Assess Performance and Aerodynamic Heating ofReusableLaunchVehicles inHypersonic Flight,"AIAA-2009-3632, Jun.2009.

Cited by 4 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

3. Review of Basic Research and Development Programs Conducted in the LENS Facilities in Hypersonic Flows;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09

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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