Unsteady boundary layer development due to wake passing effects on a highly loaded linear compressor cascade

Journal of Turbomachinery

Volumn 126, Issue 4, 2004, Pages 493-500

  Hilgenfeld, Lothar ^a   Pfitzner, Michael ^a  

^a BUNDESWEHR UNIVERSITY MUNICH   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

COMPRESSORS; DATA REDUCTION; SENSORS; TURBOMACHINE BLADES; UNSTEADY FLOW; WAKES; WIND TUNNELS;

BOUNDARY LAYER DEVELOPMENT; COMPRESSOR CASCADES; HOT-FILM ARRAYS; HOT-WIRE MEASUREMENTS;

BOUNDARY LAYERS;

BOUNDARY LAYER; COMPRESSOR; UNSTEADY FLOW; WAKE;

EID: 14744303869     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1791290     Document Type: Article

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