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Free vibration of Timoshenko beam with finite mass rigid tip load and flexural–torsional coupling
Authors:Hassan Salarieh  Mehrdaad Ghorashi  
Affiliation:aDepartment of Mechanical Engineering, Sharif University of Technology, Tehran P.O.Box 11365-9567, Iran;bThe Rotorcraft Research Group, Department of Mechanical and Aerospace Engineering, Carleton University ME3135, 1125 Colonel By Drive, Ottawa, Ont., Canada K1S 5B6
Abstract:In this paper, the free vibration of a cantilever Timoshenko beam with a rigid tip mass is analyzed. The mass center of the attached mass need not be coincident with its attachment point to the beam. As a result, the beam can be exposed to both torsional and planar elastic bending deformations. The analysis begins with deriving the governing equations of motion of the system and the corresponding boundary conditions using Hamilton's principle. Next, the derived formulation is transformed into an equivalent dimensionless form. Then, the separation of variables method is utilized to provide the frequency equation of the system. This equation is solved numerically, and the dependency of natural frequencies on various parameters of the tip mass is discussed. Explicit expressions for mode shapes and orthogonality condition are also obtained. Finally, the results obtained by the application of the Timoshenko beam model are compared with those of three other beam models, i.e. Euler–Bernoulli, shear and Rayleigh beam models. In this way, the effects of shear deformation and rotary inertia in the response of the beam are evaluated.
Keywords:Timoshenko beam  Free vibration  Rigid tip mass  Cantilever beam  Torsional deformation
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