Flow Topology About an Orbiter Leading Edge Cavity at STS-107 Reentry Conditions

Author:

Brown James1,Tobak Murray1,Prabhu Dinesh2,Sandstrom Timothy3

Affiliation:

1. NASA Ames Research Center

2. ELORET Corp.

3. AMTI

Publisher

American Institute of Aeronautics and Astronautics

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. Hypersonic Flow Computations for an Elliptic Cone at High Angle of Incidence;Journal of Spacecraft and Rockets;2012-05

2. Numerical Investigation of an Elliptic Cone at High Angle of Incidence in Nonequilibrium Flow;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04

3. Effects of Crack on Heat Flux in Hypersonic Shock/Boundary-Layer Interaction;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2010

4. Numerical Investigation of a Blunt-Nosed Elliptical Cone at High Angle of Attack in Nonequilibrium Flow;39th AIAA Fluid Dynamics Conference;2009-06-14

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