Experimental demonstration of the tip clearance flow resonance behind compressor non-synchronous vibration

Proceedings of the ASME Turbo Expo

Volumn 5, Issue PART B, 2008, Pages 653-664

  Thomassin, Jean ^a   Vo, Huu Due ^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; BLADE TIP; BLADE VIBRATIONS; EXPERIMENTAL APPARATUS; HIGH-PRESSURE COMPRESSORS; INLET TEMPERATURE; INTEGRAL MULTIPLES; LOCAL TEMPERATURE; OFF-DESIGN OPERATING CONDITIONS; ROTATIONAL FREQUENCY; ROTOR BLADES; SENSITIVITY STUDIES; SHEAR LAYER; STALL FLUTTER; STATOR BLADE; SYNCHRONOUS VIBRATION; TANGENTIAL FLOW; TEST RIGS; TEST SECTIONS; TIP CLEARANCE FLOW; TWO-BLADE; UNDERLYING MECHANISM; VIBRATORY MOTION; VORTICAL STRUCTURES;

CLOSED LOOP CONTROL SYSTEMS; COMPRESSORS; ELECTRIC MACHINERY; MINING; RESONANCE; STALL INDICATORS;

TURBOMACHINE BLADES;

EID: 69949114954     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2008-50303     Document Type: Conference Paper

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