Unsteady flow behavior due to breakdown of tip leakage vortex in an axial compressor rotor at near-stall condition

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 2000, Pages

  Furukawa, Masato ^a   Saiki, Kazuhisa ^a   Yamada, Kazutoyo ^a   Inoue, Masahiro ^a  

^a KYUSHU UNIVERSITY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; AXIAL FLOW TURBOMACHINERY; BOUNDARY LAYER FLOW; BOUNDARY LAYERS; FLOW FIELDS; FLOW OF FLUIDS; LEAKAGE (FLUID); NAVIER STOKES EQUATIONS; ROTORS; UNSTEADY FLOW; VORTEX FLOW; WALL FLOW;

ANOMALOUS PHENOMENA; AXIAL COMPRESSORS; NEAR STALL CONDITIONS; PRESSURE FLUCTUATION; SPIRAL-TYPE BREAKDOWN; THREE-DIMENSIONAL NAVIER-STOKES; TIME-AVERAGED FLOW; TIP LEAKAGE VORTEX;

FIGHTER AIRCRAFT;

EID: 84955489749     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2000-GT-0666     Document Type: Conference Paper

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