Wavelet Analysis of Wall-Pressure Fluctuations in a Supersonic Blunt-Fin Flow
Author:
Affiliation:
1. U.S. Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio 45433-7913
2. Princeton University, Princeton, New Jersey 08544-5263
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.18
Reference35 articles.
1. The unsteady characteristics of laminar juncture flow
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4. Time-sequenced and spectrally filtered Rayleigh imaging of shock wave and boundary layer structure for inlet characterization
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