Multibladerow forced response modeling in axial-flow core compressors

Journal of Turbomachinery

Volumn 129, Issue 2, 2007, Pages 412-422

  Vahdati, M ^a   Sayma, A I ^a   Imregun, M ^a   Simpson, G ^b  

^a IMPERIAL COLLEGE LONDON   (United Kingdom)

^b ROLLS ROYCE PLC   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AXIAL FLOW; DAMPING; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS; REYNOLDS EQUATION; STATORS; TURBOMACHINE BLADES; UNSTEADY FLOW; VIBRATIONS (MECHANICAL);

MULTIBLADEROW; REYNOLDS AVERAGED NAVIER-STOKE EQUATIONS; VIBRATION RESPONSE;

COMPRESSORS;

AERODYNAMICS; AXIAL FLOW; COMPRESSORS; DAMPING; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS; REYNOLDS EQUATION; STATORS; TURBOMACHINE BLADES; UNSTEADY FLOW; VIBRATIONS (MECHANICAL);

EID: 34249911990     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.2436892     Document Type: Article

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