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The effects of non-uniform temperature distribution and locally distributed anisotropic properties on thermal buckling of laminated panels

机译:温度分布不均匀和局部各向异性对层压板热屈曲的影响

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The present paper is concerned with the optimal design problem of thermal buckling for fiber reinforced laminated panels. The effects of non-uniform temperature fields and locally distributed anisotropic properties on the thermal buckling behavior are studied. In this analysis, based on the classical lamination theory in conjunction with the Hamilton's principle, the critical thermal buckling temperature difference is deduced. The numerical results show that under the non-uniform thermal loads the isotropic panel performs as anisotropic structure and it also show that the center of panel is more sensitive to the thermal effects than the edges. The effects of thermal load on panels with different boundary conditions are also investigated and it is found that the panel edges with loose constraint are more sensitive to temperature effect than with strict constraint. In the optimal fiber design problem for thermal buckling, by comparing the critical thermal buckling temperature difference of nine types of panels with different fiber distribution, it is found that the short fiber distribution can largely improve the critical thermal buckling temperature difference of fiber reinforced laminated panels. Finally, using the genetic algorithm the optimal fiber distribution is obtained for an eight-layer symmetrical panel.
机译:本文涉及纤维增强层压板热屈曲的最佳设计问题。研究了温度场不均匀和各向异性特性对热屈曲行为的影响。在此分析中,基于经典层压理论并结合汉密尔顿原理,推导出了临界热屈曲温差。数值结果表明,在非均匀热载荷下,各向同性面板表现为各向异性结构,并且还表明,面板的中心对热效应的敏感性高于边缘。还研究了热负荷对不同边界条件下的面板的影响,发现约束条件宽松的面板边缘对温度的影响要比严格约束条件下的面板边缘对温度的影响更为敏感。在热屈曲的最优纤维设计问题中,通过比较九种纤维分布不同的面板的临界热屈曲温差,发现短纤维分布可以大大改善纤维增强层压板的临界热屈曲温差。 。最后,使用遗传算法,可以获得八层对称面板的最佳纤维分布。

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