Investigation of Negative Surface Curvature Effects in Axisymmetric Shock/Boundary-Layer Interaction
Author:
Affiliation:
1. North Carolina State University, Raleigh, North Carolina 27695-7910
Funder
Air Force Office of Scientific Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J057275
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4. Unsteady wave structure near separation in a Mach 5 compression rampinteraction
5. Turbulent Properties of Axisymmetric Shock-Wave/Boundary-Layer Interaction Flows
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