3-D inviscid self-excited vibrations of a blade row in the last stage turbine

Author:

Rządkowski R.,Gnesin V.

Publisher

Elsevier BV

Subject

Mechanical Engineering

Reference18 articles.

1. Time domain flutter analysis of cascades using a full−potential solver;Bakhle;AIAA Journal,1992

2. Bendiksen, O.O., 1998. Nonlinear blade vibration and flutter in transonic rotors. In: Proceedings of ISROMAC—7, Seventh International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, February 22−26, 1998. Honolulu, Hawaii, USA, p. 664.

3. Bolcs A., Fransson, T.H., 1986. Aeroelasticity in Turbomachinesː Comparison of Theoretical and Experimental Cascade Results, Communication du LTAT−EPFL Switzerland, No. 13, p. 174.

4. Carstens, V., Belz, J., 2000. Numerical Investigation of Nonlinear Fluid–Structure Interaction in Vibrating Compressor Blades. ASME paper 2000-GT-0381.

5. Numerical modelling of aeroelastic behaviour for oscillating turbine blade row in 3D transonic ideal flow;Gnesin;Problems in Machinery Engineering,1999

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