Response of a supersonic inlet to downstream perturbations
Author:
Affiliation:
1. McDonnell Douglas Research Laboratories, St. Louis, MO
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1983-2017
Reference15 articles.
1. Sajben, M., and Kroulii, J. C. "Effeclsof Iniriol Boundary-Layer Thickness on Transonic Diffu.ser I,lows, AIAA J., v01.19.,NO.11, NOU.1981,p. 1386.
2. Bogar, T. J., Sajben, M.,and Kroulil, J. C. "CharacterisficFrequency and Length Sca 1e.iin Transonic Diffuser Flow Oscillalions,"AIAA Paper N n 81-1291, 1981, also accepledfor publicalion, AIAA J.
3. Fisher. S. A, Neule, M. C., and Brooks, A. J. "On /he .Sub-CrilicalStability of VariableRamp Intokes a1Mach NumbersAround 2, Na/ional Gas Turbine Erlablishmcnl (England)Report No. ARC-RIM-3711, Feb. 1970.
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