Experimental investigation of supersonic laminar, two-dimensional boundary-layer separation in a compression corner with and without cooling.
Author:
Affiliation:
1. California Institute of Technology, Pasadena, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.4434
Reference16 articles.
1. March 1957;Chapman D. R.
2. An experimental investigation of heat transfer effects on boundary layer separation in supersonic flow
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