Publisher
American Institute of Aeronautics and Astronautics
Reference40 articles.
1. Supersonic Inlet Shaping for Dramatic Reductions in Drag and Sonic Boom Strength
2. 2Conway, M., J., Lavely, A., W., Blaisdell. G., A. "A Computational Investigation of Flow Through an Axisymmetric SupersonicInlet,",tobe presentedatAIAAmeeting2010.
3. 3O'Brien,W.,F."DynamicSimulationofCompressorandGasTurbinePerformance",AGARD-LS-183,1992.
4. Stall Inception in Axial Flow Compressors
5. 1997 Best Paper Award—Turbomachinery Committee: A Study of Spike and Modal Stall Phenomena in a Low-Speed Axial Compressor
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