An Integrated Nonlinear Approach for Turbomachinery Forced Response Prediction. Part II: Case Studies

Journal of Fluids and Structures

Volumn 14, Issue 1, 2000, Pages 103-125

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

^a IMPERIAL COLLEGE LONDON   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0001452041     PISSN: 08899746     EISSN: None     Source Type: Journal    
DOI: 10.1006/jfls.1999.0254     Document Type: Article

References (6)

1. EDMONDS J. D. Recent developments in the application of Laser Doppler anemometry to compressor rigs. Symposium on Advanced Non-intrusive Instrumentation for Probulsion Engines. 1997;AGARD.
2. GREEN J. S., MARSHALL J. G. Forced response predictions within the design process. 3rd European Conference on Turbomachinery. 1999;. p. 377-391.
3. SANLITURK K. Y., EWINS D. J. Modelling two-dimensional friction contact and its application using harmonic balance method. Journal of Sound and Vibration. 193:1996;511-523.
4. SAYMA A. I., VAHDATI M., GREEN J. S., IMREGUN M. Whole assembly flutter analysis of a low-pressure turbine blade. 3rd National Turbine Engine High Cycle Fatigue Conference. 1998;San Antonio, Texas.
5. SBARDELLA L., SAYMA A. I., IMREGUN M. Semi-unstructured mesh generator for flow calculations in axial turbomachinery blading. Fransson T. 18th International Symposium on Unsteady Aerodynamics and Aeroelasticity of Turbomachines. 1997;Kluwer Academic Publishers, Dordrecht.
6. SAYMA A. I., VAHDATI M., IMREGUN M. An integrated nonlinear approach for turbomachinery forced response prediction. Part I: formulation. Journal of Fluids and Structures. 14:2000;87-101.