Experimental investigation of the effects of wall suction and blowing on the performance of highly offset diffusers
Author:
Affiliation:
1. Boeing Military Airplane Co., Seattle, WA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1983-1169
Reference3 articles.
1. An approach to conformal inlet diffuser design for integrated propulsion systems
2. Combined Viscous-Inviscid Analysis of Supersonic Inlet Flowfields
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