Boundary-layer Separation Detection for a Cone at High Angle of Attack in Mach 4.5 Flow with Pressure-Sensitive Paint
Author:
Affiliation:
1. University of Notre Dame
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-3120
Reference39 articles.
1. Boundary-Layer Transition Experiment During Reentry of HIFiRE-1
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5. 5Tracy, R. R., Hypersonic Flow over a Yawed Circular Cone, Ph.D. thesis,California Institute of Technology, Pasadena, CA, August 1963.
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