AIAA-2005-1054 UNSTEADY BOUNDARY LAYER DEVELOPMENT DUE TO WAKE PASSING EFFECTS ON A HIGHLY LOADED LINEAR COMPRESSOR CASCADE
17th, International symposium on air breathing engines ; 2005 ; Munich, Germany
01.01.2005
38 pages
Includes bibliographical references and index; Papers on CD-ROM
Aufsatz (Konferenz)
Englisch
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