Nonlinear Vibrations of Cantilever Beams and Plates

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Chapter 1.1 Motivation:
The beam is one of the fundamental elements of an engineering structure. It finds use in varied;structural applications. Moreover, structures like helicopter rotor blades, spacecraft antennae, flexible;satellites, airplane wings, gun barrels, robot arms, high-rise buildings, long-span bridges, and subsystems;of more complex structures can be modeled as a beam-like slender member. Therefore, studying;the static and dynamic response, both theoretically and experimentally, of this simple structural component;under various loading conditions would help in understanding and explaining the behavior of;more complex, real structures under similar loading.;Interesting physical phenomena occur in structures in the presence of nonlinearities, which cannot;be explained by linear models. These phenomena include jumps, saturation, subharmonic, superharmonic,;and combination resonances, self-excited oscillations, modal interactions, and chaos. In reality,;no physical system is strictly linear and hence linear models of physical systems have limitations of;their own. In general, linear models are applicable only in a very restrictive domain like when the;vibration amplitude is very small. Thus, to accurately identify and understand the dynamic behavior;of a structural system under general loading conditions, it is essential that nonlinearities present in the;system also be modeled and studied.;In continuous (or distributed-parameter) systems like structures, nonlinearities essentially couple;;the linearly uncoupled normal modes, and this coupling could lead to modal interactions (i.e., interaction;between the modes), resulting in the transfer of energy among modes. Experiments have;demonstrated that sometimes energy is transferred from a directly excited high-frequency mode to a;low-frequency mode, which may be extremely dangerous because the response amplitude of the lowfrequency;mode can be very large compared with that of the directly