In this study, the dynamic response behavior of curvilinear fibers based layered-composite beam under transversely moving load is investigated considering linear and nonlinear analyses. The formulation is developed applying sinusoidal shear flexible beam theory, geometrical nonlinearity based on von Kármán’s assumption, and the constitutive equation fulfilling the plane stress situation through the width of arbitrarily lay-up composite beam. The load on the beam is treated as moving with uniform velocity, acceleration and also oscillatory motion with time. The governing nonlinear dynamic equations are framed employing Hamilton’s principle and by adopting finite element approach. The response of beam in time domain is obtained solving the governing equations through direct time integration method by Newmark integration scheme. and the results are viewed through the frequency-amplitude relationship. A detailed parametric study involving curvilinear fiber path angles, lay-up ply angles, thickness ratio, moving load velocity, and acceleration, and forcing frequency is made on the dynamic behavior of variable stiffness beam with curvilinear fiber beam. The effect of thermal environment and boundary conditions on the vibrational response behavior of beam is also predicted.
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