Acoustic-wave/blade-row interactions establish boundary conditions for unsteady inlet flows

Journal of Propulsion and Power

Volumn 17, Issue 5, 2001, Pages 1090-1099

  Sajben, M ^a   Said, H ^a  

^a UNIVERSITY OF CINCINNATI   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC WAVE REFLECTION; BOUNDARY CONDITIONS; COMPRESSORS; COMPUTER SIMULATION; FLOW INTERACTIONS; TURBOMACHINE BLADES;

INLET FLOWS;

UNSTEADY FLOW;

EID: 0035443336     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5848     Document Type: Article

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