Experimental Investigation of High-Enthalpy Effects on Attachment-Line Boundary-Layer Transition
Author:
Affiliation:
1. National Aerospace Laboratory, Tokyo 182-8522, Japan
2. California Institute of Technology, Pasadena, California 91125
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2096
Reference32 articles.
1. Transition of compressible high enthalpy boundary layer flow over a flat plate
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4. Real gas effects on hypersonic boundary‐layer stability
5. Linear disturbances in hypersonic, chemically reacting shock layers
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