Holographic interferometry study of an axisymmetric shock-wave/boundary-layer strong interaction flow
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California
2. University of Missouri, Columbia, Missouri
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9621
Reference12 articles.
1. The Structure of Turbulence in a Supersonic Shock-Wave/Boundary-Layer Interaction
2. Prediction of Transonic Separated Flows
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