Downstream boundary effects on the frequency of self-excited oscillations in transonic diffuser flows
Author:
Affiliation:
1. U.S. Navy, Naval Surface Weapons Center, Silver Spring, MD
2. NASA, Ames Research Center, Moffett Field, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1987-161
Reference13 articles.
1. Experimental Investigation of Pressure Oscillations in a Side Dump Ramjet Combustor
2. Characteristic frequencies of transonic diffuser flow oscillations
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