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

Proceedings of the ASME Turbo Expo

Volumn 4, Issue , 2000, Pages

  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; ASPECT RATIO; DAMPING;

AERODYNAMIC DAMPING; BLADE FLEXIBILITY; INLET DISTORTION; LOW ASPECT RATIO; RESONANT CONDITION; STANDARD FINITE ELEMENT; UNSTEADY PRESSURE DISTRIBUTION; UNSTEADY PRESSURES;

FINITE ELEMENT METHOD;

EID: 84955295454     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2000-GT-0373     Document Type: Conference Paper

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