Unsteady Aerodynamic Flow Phenomena in a Transonic Compressor Stage
Author:
Affiliation:
1. NASA Lewis Research Center, Cleveland, Ohio 44135
2. U.S. Air Force Wright Laboratory, Wright–Patterson Air Force Base, Ohio 45433
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/10.2514/2.5175
Reference19 articles.
1. Prediction of Compressor Cascade Performance Using a Navier–Stokes Technique
2. The Use of a Distributed Body Force to Simulate Viscous Effects in 3D Flow Calculations
3. A Numerical Modeling of Endwall and Tip-Clearance Flow of an Isolated Compressor Rotor
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