Experimental Investigation of Microramp Control of an 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.J057846
Reference39 articles.
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4. WietingA. R. “Exploratory Study of Transient Unstart Phenomena in a Three-Dimensional Fixed-Geometry Scramjet Engine,” NASA TN D-8156l, 1976.
5. Experimental Investigation of Unstart in an Inlet/Isolator Model in Mach 5 Flow
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