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- W3133750345 abstract "Abstract Coriolis forces, on a blade mounted on a disc rotating with angular acceleration, give rise to a pseudo static excitation to the blade. The resulting vibrations are simultaneously influenced by the changing stiffness of the blade under acceleration. The occurrence of this shock phenomenon has been reported in earlier studies for uniform beams. In this paper the phenomenon is investigated for a typical tapered, pretwisted, turbine lade with an asymmetric aerofoil cross section and mounted on the disc at a stagger angle. The governing equations of motion, for uniform rates of acceleration are derived employing Lagrangian equations. The vibration response patterns of the blade, obtained numerically, for typical acceleration rates are illustrated." @default.
- W3133750345 created "2021-03-15" @default.
- W3133750345 creator A5060542297 @default.
- W3133750345 date "1995-09-17" @default.
- W3133750345 modified "2023-09-25" @default.
- W3133750345 title "Pseudo Static Excitation of Turbine Blades Under Acceleration" @default.
- W3133750345 cites W2086223266 @default.
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- W3133750345 doi "https://doi.org/10.1115/detc1995-0515" @default.
- W3133750345 hasPublicationYear "1995" @default.
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