Numerical Investigation of Inlet Distortion on an Axial Flow Compressor Rotor with Circumferential Groove Casing Treatment
CHINESE JOURNAL OF AERONAUTICS ; 21 , 6 ; 496-505
01.01.2008
10 pages
Aufsatz (Zeitschrift)
Englisch
DDC: | 629.13 |
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Experimental Investigation of Circumferential Grooved Casing/Hub Treatment in Axial Flow Compressor
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