Control of Compressor Face Total Pressure Distortion on a High Bypass Turbofan Intake Using Air-Jet Vortex Generators
Author:
Affiliation:
1. University of Manchester
2. Laboratoire de Metrologie des Oscillateurs
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2206
Reference34 articles.
1. Internal cowl-separation at high incidence angles
2. Prediction of Boundary-Layer Flow Separation in V/STOL Engine Inlets
3. Design and Experimental Studies of a Type A V/STOL Inlet
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