Recommendations for Hypersonic Boundary Layer Transition Flight Testing
Author:
Affiliation:
1. NASA Langley Research Center
2. Air Force Research Laboratory
3. Case Western Reserve University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3415
Reference73 articles.
1. Influence of Laminar Boundary-Layer Transition on Entry Vehicle Designs
2. Flight Data for Boundary-Layer Transition at Hypersonic and Supersonic Speeds
3. Reshotko,E."BoundaryLayerInstability,Transition,andControl,"AIAAPaper94-0001,Jan.1994.
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