Prediction of compressor stall for distorted and undistorted flow byuse of a multistage compressor simulation on the digital computer
13th Aerospace Sciences Meeting ; 1975 ; Pasadena , CA , U.S.A.
1975-01-01
Conference paper
Electronic Resource
English
Prediction of the Stall Boundary in Multistage Axial Flow Compressor
British Library Online Contents | 1996
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Online Contents | 1995
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