Compressor blade row unsteady aerodynamic response to attached and separated flow forcing functions
30th Aerospace Sciences Meeting and Exhibit ; 1992 ; Reno , NV , U.S.A.
1992-01-01
Conference paper
Electronic Resource
English
Axial Compressor Blade-to-Blade Unsteady Aerodynamic Variability
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|Separated flow unsteady aerodynamic theory
AIAA | 1985
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