Structure and Oscillation Phenomena of Pseudo-Shock Waves in a Straight Square Duct at Mach 2 and 4
Author:
Affiliation:
1. Muroran Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-2646
Reference14 articles.
1. Shock train and pseudo-shock phenomena in internal gas flows
2. Fluid Phenomena in Scramjet Combustion Systems
3. Characteristics of multiple shock wave/turbulent boundary-layer interactions in rectangular ducts
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