The tip clearance flow resonance behind axial compressor nonsynchronous vibration

Journal of Turbomachinery

Volumn 133, Issue 4, 2011, Pages

  Thomassin, Jean ^a   Vo, Huu Duc ^b   Mureithi, Njuki W ^b  

^a PRATT AND WHITNEY CANADA   (Canada)

^b ÉCOLE POLYTECHNIQUE DE MONTRÉAL   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC FEEDBACK; AXIAL COMPRESSORS; BLADE TIP; BLADE VIBRATIONS; EXPERIMENTAL APPARATUS; EXPERIMENTAL CONFIRMATION; HIGH PRESSURE COMPRESSOR; INLET TEMPERATURE; LOCAL TEMPERATURE; NON INTEGRALS; NONSYNCHRONOUS VIBRATIONS; OFF-DESIGN OPERATING CONDITIONS; ROTATIONAL FREQUENCY; ROTOR BLADES; SENSITIVITY STUDIES; SHEAR LAYER; STALL FLUTTER; STATOR BLADE; SURFACE PRESSURES; TANGENTIAL FLOW; TEST RIGS; TIP CLEARANCE FLOW; TWO-BLADE; UNDERLYING MECHANISM; VIBRATORY MOTION; VORTICAL STRUCTURES;

COMPRESSORS; HELICOPTER ROTORS; RESONANCE; STALL INDICATORS; TURBOMACHINE BLADES; UNSTEADY FLOW;

SHEAR FLOW;

EID: 79955438818     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.4001368     Document Type: Article

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