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Stability and Free Vibration Behaviour of Laminated Composite Panels Under Thermo-mechanical Loading

机译:层压复合板在热机械载荷下的稳定性和自由振动行为

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In this article, the free vibration and the buckling (mechanical and/or thermal) behaviour of laminated composite flat and curved panels are analysed numerically. Simulation model has been developed using ANSYS Parametric design language code in the ANSYS environment. The convergence behaviour of present finite element results have been checked and comprehensiveness of the model is revealed by comparing the results with those available published literature. Wide variety of numerical examples is solved for different parameters such as lamination schemes, support conditions and material properties under the thermo-mechanical load to highlight the applicability of the present simulation model. It is finally understood that the proposed model is capable of solving the mechanical responses (free vibration and buckling) of orthotropic materials accurately with very less computational cost under the combined action of loading.
机译:在本文中,数值分析了层压复合平板和弯曲面板的自由振动和屈曲(机械和/或热)行为。在ANSYS环境中使用ANSYS Parametric设计语言代码开发了仿真模型。目前的有限元结果的收敛行为已经过检查,并且通过将结果与现有文献进行比较,揭示了模型的全面性。针对不同参数(例如叠层方案,支撑条件和热机械载荷下的材料特性)求解了各种数值示例,以突出本仿真模型的适用性。最终可以理解,所提出的模型能够在载荷的共同作用下以非常少的计算成本来精确求解正交各向异性材料的机械响应(自由振动和屈曲)。

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