Investigation of a Cascade with Controlled Duffusion Airfoils Designed for an Inlet Mach Number of 0.92

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H. A. Schreiber,W. Steinert,H. Starken-1992-01-01-elib (German Aerospace Center)

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Mach numberCascadeInletAirfoilDrag divergence Mach numberAerospace engineeringAcousticsMechanics

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