Shock-Wave Oscillations in a Transonic Diffuser Flow
Author:
Affiliation:
1. McDonnell Douglas Corporation, St. Louis, Mo.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.61280
Reference10 articles.
1. A high-speed schlieren investigation of diffuser flows with dynamic distortion
2. Pressure Fluctuations Beneath Turbulent Boundary Layers
3. Fluctuating Wall Pressure under a Separated Supersonic Flow
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