An integrated time-domain aeroelasticity model for the prediction of fan forced response due to inlet distortion

Journal of Engineering for Gas Turbines and Power

Volumn 124, Issue 1, 2002, Pages 196-208

  Breard C ^a   Vahdati, M ^a   Sayma, A I ^a   Imregun, M ^a  

^a IMPERIAL COLLEGE LONDON   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BOUNDARY CONDITIONS; DAMPING; PRESSURE DISTRIBUTION; TURBOMACHINE BLADES; UNSTEADY FLOW;

TRANSONIC FAN;

FANS;

AEROELASTICITY; FAN; INLET; TRANSONIC FLOW;

EID: 0036461904     PISSN: 07424795     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1416151     Document Type: Article

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