A third-order shear deformation plate bending formulation for thick plates: first principles derivation and applications

Q4 Engineering
Charles Chinwuba Ike
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引用次数: 0

Abstract

A third-order shear deformation plate bending formulation is presented in this study from the first principles. The derivation assumed a displacement field constructed using third-order polynomial function of the transverse (z) coordinate; and made to apriori satisfy the linear three-dimensional (3D) kinematics relations as well as the transverse shear stress free boundary conditions at the top and bottom plate surfaces. The formulation thus has no need for shear stress correction factors of the first-order shear deformation plate theories. The domain equations of equilibrium are obtained as a set of three coupled differential equations in terms of three unknown displacements. The system of coupled equations is solved for simply supported rectangular and square plates subjected to four cases of loading distributions: sinusoidal loading, uniformly distributed loading, linearly distributed loading and point load at the plate center. Navier’s double trigonometric series method is used to construct trial solutions for the three displacement functions such that the boundary conditions are satisfied identically. The integration problem is thus reduced to an algebraic problem and is solved for each considered loading. It is found that the present formulation gives exact results for the normal stresses σxx for sinusoidal and uniformly distributed loads. The study further showed that the results for deflection and stresses agreed with Krishna Murty’s higher order shear deformation plate theory results. The present formulation gave accurate results because of the inclusion of transverse normal strain effects in the formulation. The formulation gives a quadratic variation of the transverse shear stresses across the thickness in consonance with the theory of elasticity method.
厚板的三阶剪切变形板弯曲公式:第一原理推导与应用
本研究从第一性原理出发,提出了三阶剪切变形板弯曲公式。推导假定位移场使用横向(z)坐标的三阶多项式函数构造,并先验地满足线性三维(3D)运动学关系以及板顶部和底部表面的横向无剪应力边界条件。因此,该公式不需要一阶剪切变形板理论的剪应力修正系数。平衡域方程是由三个未知位移组成的三个耦合微分方程构成的。该耦合方程组用于求解受到四种荷载分布情况(正弦荷载、均匀分布荷载、线性分布荷载和板中心点荷载)作用的简单支撑矩形板和正方形板。Navier 双三角级数法用于构建三个位移函数的试解法,从而使边界条件完全一致。因此,积分问题被简化为代数问题,并针对每种考虑的载荷进行求解。研究发现,对于正弦荷载和均匀分布荷载,本公式给出了法向应力 σxx 的精确结果。研究进一步表明,挠度和应力结果与 Krishna Murty 的高阶剪切变形板理论结果一致。由于公式中包含了横向法向应变效应,因此本公式给出了精确的结果。该公式给出了横向剪应力在厚度上的二次变化,与弹性理论方法一致。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
CiteScore
0.10
自引率
0.00%
发文量
8
审稿时长
10 weeks
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