Volumetric Measurement of a Shock Wave-Turbulent Boundary Layer Interaction Using Plenoptic Particle Image Velocimetry
Author:
Affiliation:
1. Auburn University
2. Florida State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-4029
Reference20 articles.
1. 50 years of shock wave/boundary layer interaction research - What next?
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