A COUPLED FLUID–STRUCTURE ANALYSIS FOR 3-D INVISCID FLUTTER OF IV STANDARD CONFIGURATION

Author:

GNESIN V.,RZĄDKOWSKI R.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference14 articles.

1. A. BÖLCS, T. H. FRANSSON, 1986, Communication du LTAT-EPFL Switzerland, 13, Aeroelasticity in turbomachines: comparison of theoretical and experimental cascade results

2. F. MOYROUD, G. JACQUET-RICHARDE, T. H. FRANSSON, 1996, ASME Paper 96-GT-335, 1, 19, A modal coupling for fluid and structure analysis of turbomachines flutter application to a fan stage

3. Time domain flutter analysis of cascades using a full-potential solver;BAKHLE;American Institute of Aeronautics and Astronautics Journal,1992

4. Nonlinear blade vibration and flutter in transonic rotors;BENDIKSEN;Proceedings of ISROMAC-7, The Seventh International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, Honolulu, HI, U.S.A,1998

5. Transonic bending flutter in rotors and cascades;BENDIKSEN;The Nineth International Symposium of Unsteady Aerodynamics and Aeroelasticity of Turbomachines, Book of Abstracts, Lyon, France, September 4–8,2000

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