A method for forced response analysis of mistuned bladed disks with aerodynamic effects included

Journal of Engineering for Gas Turbines and Power

Volumn 132, Issue 6, 2010, Pages 62502-1-62502-10

  Petrov, E P ^a  

^a IMPERIAL COLLEGE LONDON   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC DAMPING; AERODYNAMIC EFFECT; AERODYNAMIC FORCES; BLADE VIBRATIONS; BLADED DISK; BLADED-DISK MODELS; FLEXIBLE DISKS; FORCED RESPONSE; FORCED RESPONSE ANALYSIS; FREQUENCY RESPONSE FUNCTION MATRIXES; FREQUENCY VEERING; GAS FLOWS; HIGH-ACCURACY; MECHANICAL COUPLING; MISTUNED; MISTUNING; VIBRATING BLADE;

AERODYNAMICS; DISKS (MACHINE COMPONENTS); FLOW OF GASES; FREQUENCY RESPONSE; TURBOMACHINE BLADES; VIBRATIONS (MECHANICAL);

DISKS (STRUCTURAL COMPONENTS);

EID: 78149374016     PISSN: 07424795     EISSN: 15288919     Source Type: Journal    
DOI: 10.1115/1.4000117     Document Type: Article

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