Hypersonic Reentry Vehicle Wake Flow Fields at Angle of Attack
Author:
Affiliation:
1. Northrop Grumman Corporation
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-582
Reference48 articles.
1. 1Martelluci,A."ExperimentalStudyofNearWakes,"BSD-TR-67-229-Vol.1.DataPresentation, November1967.
2. 3Conti,Raul,"NumericalMethodforBaseandWakeFlowAnalysis,"DET10TR94-22,January
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