Coupled bending-torsion vibrations of rotating blades of asymmetric aerofoil cross section with allowance for shear deflection and rotary inertia by use of the Reissner method

DOI10.1016/0022-460X(81)90233-9zbMath0449.73067OpenAlexW2014046768MaRDI QIDQ3896616

Satish V. Kulkarni, K. B. Subrahmanyam

Publication date: 1981

Published in: Journal of Sound and Vibration (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0022-460x(81)90233-9

zbMATH Keywords

rotary inertiafrequency equationsshear deflectionrotating bladesReissner methodasymmetric aerofoil cross sectioncoupled bending-torsion vibrationsshape functions are developed in series form

Mathematics Subject Classification ID

Vibrations in dynamical problems in solid mechanics (74H45) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

Related Items (4)

Nonlinear vibrations of blade with varying rotating speed ⋮ Energy expressions and free vibration analysis of a rotating double tapered Timoshenko beam featuring bending-torsion coupling ⋮ Flexural-flexural-torsional Nonlinear Vibrations of Pre-twisted Rotating Beams with Asymmetric Cross-sections ⋮ Nonlinear dynamic responses of rotating pretwisted cylindrical shells

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