Active Flow Control on a Non-steady Operated Compressor Stator Cascade by Means of Fluidic Devices
German aerospace aerodynamics and the german society for aeronautics and astronautics (Symposium)
German aerospace aerodynamics and the german society for aeronautics and astronautics (Symposium) ; 337-348
01.01.2018
12 pages
Aufsatz (Konferenz)
Englisch
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