Experimental investigation of separated flow over a cavity at hypersonic speed.
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.5280
Reference13 articles.
1. Heat Transfer in Separated Flows
2. A study of laminar hypersonic cavity flows
3. Momentum integral methods for the laminar free shear layer
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