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- W2978779093 abstract "Flutter calculations for turbomachinery blade rows often employ the energy method and Lane′s traveling wave model in which the adjacent blades in a blade row are assumed to vibrate at the same frequency but with a constant phase difference,called interblade phase angle(IBPA).With this model,aerodynamic responses of the blade row can be determined by using a single blade passage to minimize the computational effort.Consequently,a phase-shifted periodic boundary condition has to be applied when the IBPA is not zero.Compared with the experiments results of NASA Rotor67 and the fourth standard configuration(STCF4),the unsteady aerodynamics and aeroelastic behaviors are described,and the flutter predictions are performed according to the damping coefficient based on the energy method." @default.
- W2978779093 created "2019-10-10" @default.
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- W2978779093 date "2009-01-01" @default.
- W2978779093 modified "2023-09-23" @default.
- W2978779093 title "Flutter Computation of Turbomachinery Blades Based on CFD" @default.
- W2978779093 hasPublicationYear "2009" @default.
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