An analysis system for blade forced response

Journal of Turbomachinery

Volumn 115, Issue 4, 1993, Pages 762-770

  Chiang, Hsiao Wei D ^a   Kielb, R E ^a  

^a GE AVIATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; MATHEMATICAL MODELS; SHOCK WAVES; TURBINES;

BLADE FORCED RESPONSE; CAMPBELL DIAGRAM; FLOW FIELD; INLET DISTORTION;

TURBOMACHINERY;

EID: 0027680765     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2929314     Document Type: Article

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