A numerical modelling of stator–rotor interaction in a turbine stage with oscillating blades

Author:

Gnesin V.I.,Kolodyazhnaya L.V.,Rzadkowski R.

Publisher

Elsevier BV

Subject

Mechanical Engineering

Reference11 articles.

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

2. Bolcs, A., Fransson, T.H., 1986. Aeroelasticity in turbomachines: comparison of theoretical and experimental cascade results, Communication du LTAT-EPFL, Switzerland, No. 13, p. 174.

3. Part-speed flutter analysis of a wide-chord fan blade;Chew,1998

4. Gnesin, V.I., 1982. The calculation of three-dimensional transonic gas flow through the axial turbine stage. News of USSR Academy of Science, Gas and Fluid Mechanics, Moscow, No. 6, pp. 138–146 (in Russian).

5. A numerical study of 3-D flutter in turbomachines using fluid–structure coupled method;Gnesin;Engineering Mechanics,1999

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