Effects of Endwall Boundary Layers on the Performance of a Subsonic Axial Inlet Flow Compressor Rotor
18th Aerospace ground testing conference ; 1994 ; Colorado Springs; CO
18th Aerospace ground testing conference ; aiaa 94-2691 ; ALL
PAPERS- AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS ; aiaa 94-2691
1994-01-01
ALL
Papers AIAA-94-2500 - 2699 with gaps held only
Conference paper
English
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3D ENDWALL PROFILING IMPACT ON AXIAL FLOW COMPRESSOR AERODYNAMICS
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