Control of Incident Shock/Boundary-Layer Interaction by a Two-Dimensional Bump
Author:
Affiliation:
1. College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052786
Reference31 articles.
1. Progress in Astronautics and Aeronautics;Van Wie D. M.,2000
2. Intake Aerodynamics, Second Edition
3. Experimental Investigation of the Internal Compression Inside a Hypersonic Intake
4. Shock-Wave/Boundary-Layer Interactions in a Model Scramjet Intake
5. AndersonB. H. “Design of Supersonic Inlets by a Computer Program Incorporation the Method of Characteristics,” NASA TN-D-4960, 1968.
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