A numerical method for the prediction of bladed disk forced response

Journal of Engineering for Gas Turbines and Power

Volumn 119, Issue 2, 1997, Pages 404-410

  Berthillier, M ^a   Dhainaut, M ^a   Burgaud, F ^a   Gamier, V ^a  

^a SNECMA   (France)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0013320921     PISSN: 07424795     EISSN: 15288919     Source Type: Journal    
DOI: 10.1115/1.2815589     Document Type: Article

References (13)

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2. Crawley, E. F., 1988, “Aeroelastic Formulation for Tuned and Mistuned Rotors,” AGARD Manual on Aeroelasticity in Axial-Flow Turbomachines, Vol. 2, Structural Dynamics and Aeroelasticity.
3. Davis, P. J., 1979, Circulant Matrices, Wiley-Interscience.
4. Ferraris, G., Henry, R., Lalanne, M., and Trompette, P., 1983, “Frequencies and Mode Shapes of Rotating Bladed Axisymmetric Structures. Application to a Jet Engine,” Advanced Vibrations of Bladed Disc Assemblies, ASME, 10 pp.
5. Fleeter, S., 1992, “Forced Response Unsteady Aerodynamic Experiments,” AIAA Paper No. 92-0144.
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9. Joubert, H., and Ronchetti, V., 1989, “Aerodynamic Study of Forced Vibrations on Stator Rows of Axial Compressors,” AGARD CP 468; Unsteady Aerodynamic Phenomena in Turbomachines, Aug.
10. Murthy, D. V., and Stefko, G. L., 1992, “FREPS: A Forced Response Prediction System for Turbomachinery Blade Rows,” AIAA Paper No. 92-3072.
11. Tatakis, S., and Stockton, R., 1993, “Structural and Aerodynamic Influences to Airfoil Forced Response,” ASME Paper No. 93-GT-243.
12. Verdon, J. M., 1993, “Review of Unsteady Aerodynamic Methods for Turbomachinery Aeroelastic and Aeroacoustic Applications,” AIAA Journal, Vol. 31, No. 2, pp. 235-250.
13. Wildheim, S. J., 1979, “Excitation of Rotationally Periodic Structures,” ASME Journal of Applied Mechanics, Vol 46, pp. 878-882.