Skin-friction measurements in three-dimensional, supersonic shock-wave/boundary-layer interaction
Author:
Affiliation:
1. University of Missouri, Columbia, Missouri 65201
2. NASA Ames Research Center, Moffett Field, California 94035
3. Istanbul Technical University, 80626 Istanbul, Turkey
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12503
Reference20 articles.
1. Holographic interferometry study of an axisymmetric shock-wave/boundary-layer strong interaction flow
2. Two-component LDV investigation of three-dimensional shock/turbulentboundary-layer interactions
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