Influence of tip-clearance, aspect ratio, blade loading, and inlet boundary layer on secondary losses in compressor cascades

ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition, GT 1996

Volumn 1, Issue , 1996, Pages

  Hübner, Jürgen ^a   Fottner, Leonhard ^a  

^a BUNDESWEHR UNIVERSITY MUNICH   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; BOUNDARY LAYERS; CASCADES (FLUID MECHANICS); COMPRESSORS; GAS TURBINES; INLET FLOW; NAVIER STOKES EQUATIONS; WAKES;

COMPRESSOR CASCADE; DISPLACEMENT THICKNESS; INLET BOUNDARY LAYER; LOSS COEFFICIENTS; RADIAL DISTRIBUTIONS; SURFACE FLOW VISUALIZATION; THREE DIMENSIONAL FLOW FIELD; TIP CLEARANCE VORTEX;

ASPECT RATIO;

EID: 84923887038     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/96-GT-505     Document Type: Conference Paper

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