Upstream-Propagating Potential Disturbances Interacting with A Compressible Cascade
Author:
Affiliation:
1. U.S. Air Force Academy, Colorado Springs, Colorado 80840
2. University of Notre Dame, South Bend, Indiana 46556
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.5762
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1. Multistage Axial-Flow Turbomachine Wake Production, Transport, and Interaction
2. An Investigation of Axial Compressor Rotor Aerodynamics
3. Measurement and Analysis of Total-Pressure Unsteadiness Data From an Axial-Flow Compressor Stage
4. Blade-Row Interaction in an Axial-Flow Subsonic Compressor Stage
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