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Thermo-mechanical vibration analysis of rotating nonlocal nanoplates applying generalized differential quadrature method

机译:旋转非局部纳米板的热机械振动分析应用广义差分正交方法

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摘要

In this study, thermal and small-scale effects on the flapwise bending vibrations of a rotating nanoplate, which can be the basis of nano-turbine design, have been analyzed. The nano-turbine is made of an orthotropic nanoplate with a setting angle that is modeled based on the classical plate theory (CPT) with cantilever boundary conditions. The axial forces are also included in the model as the true spatial variation due to the rotation and temperature change. The governing equations and boundary conditions are derived according to Hamilton's principle and the governing equations are solved with the aid of the generalized differential quadrature method. The effects of small-scale parameter, nondimensional angular velocity, temperature change, and setting angles in the first four nondimensional frequencies are discussed. Due to the consideration of the rotating effects, results of this study are applicable in nano-machines, such as nano-motors, nano-rotor, and other rotating nano-structures. Also, by considering the effect of thermal loading on rotation of a nanoplate, the results are useful in the design of nano-turbines.
机译:在本研究中,已经分析了对旋转纳米板的浮动弯曲振动的热和小规模效应,其可以是纳米涡轮设计的基础。纳米涡轮机由正交纳米板制成,其具有基于悬臂边界条件的经典板理论(CPT)建模的设定角度。由于旋转和温度变化,轴向力也包括在模型中作为真正的空间变化。根据汉密尔顿的原理和借助于广义差分正交方法解决了管理方程和边界条件。讨论了小规模参数,非尺寸角速度,温度变化和在前四个非潜能频率中的设定角度的影响。由于考虑了旋转效应,本研究的结果适用于纳米机,例如纳米电动机,纳米转子和其他旋转纳米结构。而且,通过考虑热负荷对纳米板旋转的影响,结果可用于纳米涡轮机的设计。

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