Flapwise bending vibration analysis of a rotating double-tapered Timoshenko beam |
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Authors: | O. Ozdemir Ozgumus M. O. Kaya |
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Affiliation: | (1) Istanbul Technical University, Faculty of Aeronautics and Astronautics, 34469 Maslak, Istanbul, Turkey |
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Abstract: | In this study, free vibration analysis of a rotating, double-tapered Timoshenko beam that undergoes flapwise bending vibration is performed. At the beginning of the study, the kinetic- and potential energy expressions of this beam model are derived using several explanatory tables and figures. In the following section, Hamilton’s principle is applied to the derived energy expressions to obtain the governing differential equations of motion and the boundary conditions. The parameters for the hub radius, rotational speed, shear deformation, slenderness ratio, and taper ratios are incorporated into the equations of motion. In the solution, an efficient mathematical technique, called the differential transform method (DTM), is used to solve the governing differential equations of motion. Using the computer package Mathematica the effects of the incorporated parameters on the natural frequencies are investigated and the results are tabulated in several tables and graphics. |
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Keywords: | Nonuniform Timoshenko beam Tapered Timoshenko beam Rotating Timoshenko beam Differential transform method Differential transformation |
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