Blade forced response prediction for industrial gas turbines part 2: Verification and application

American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) IGTI

Volumn 4, Issue , 2003, Pages 415-422

  Ning, Wei ^a   Moffatt, Stuart ^b   Li, Yansheng ^a   Wells, Roger G ^a  

^a Alstom UK   (United Kingdom)

^b DURHAM UNIVERSITY   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

BLADE FORCED RESPONSE PREDICTION; MODAL REDUCTION METHODS;

ACCELERATION; AERODYNAMICS; COMPUTATIONAL FLUID DYNAMICS; DAMPING; FINITE ELEMENT METHOD; INTERPOLATION; NATURAL FREQUENCIES; PRESSURE DISTRIBUTION; STRAIN GAGES; TURBOMACHINE BLADES; UNSTEADY FLOW; VIBRATIONS (MECHANICAL);

GAS TURBINES;

EID: 0347596562     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2003-38642     Document Type: Conference Paper

References (13)

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4. Silkowski, P. D., Rhie, C. M., Copeland, G. S., Eley, J. A., Bleeg, J. M., 2001, "CFD Investigation of Aeromechanics", ASME 2001-GT-0267
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9. rd European Conference on Turbomachinery, pp. 271-287
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12. Li, Y. S. and Wells, R. G., 1999, " The Three-Dimensional Aerodynamic Design and Test of a Three-Stage Transonic Compressor", ASME 99-GT-068
13. Kielb, R. E. and Imregun, M., 1999, "Aeroelasticity in Axial Flow Turbomachines - Damping Characteristics", VKI Lecture Series 1999-05, von Karman Institute for Fluid Dynamics, Belgium