考虑横向剪切弱抗力的柔性加筋板粘弹塑性变形建模

A. P. Yankovskii
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引用次数: 5

摘要

基于时间步长算法,建立了平行于中平面交叉加筋柔性板粘弹塑性变形的数学模型。假定板的组成构件的变形较小,并将其分解为弹性构件和塑性构件。复合材料的粘弹性行为服从于麦克斯韦-玻尔兹曼体的关系。非弹性变形由各向同性硬化塑性流动理论方程定义。横向的法向应力随板的厚度线性近似。因此,在横向上的线性变形及其速度被排除在组成分量的控制方程之外。在非经典Reddy弯曲理论的框架下,考虑了纤维板横向剪切抗力的减弱。在卡门近似中考虑了问题的几何非线性。采用“交叉”型的显式格式,对公式化的初边值问题进行了数值求解。为了得到稳定的数值格式,采用了一种人工方法:将当前离散时刻麦克斯韦-玻尔兹曼粘弹性关系中的应力用带退步的梯形公式表示为应力速度。研究了较厚正交增强玻璃纤维矩形板在爆炸载荷作用下的弹塑性和粘弹塑性弯曲动力特性。结果表明,配筋结构的变化会引起结构残余挠度值的变化。结果表明,加筋板在初始时间瞬间附近的振动幅值明显大于残余挠度值。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Modelling the viscoelastic-plastic deformation of flexible reinforced plates with account of weak resistance to transverse shear
A mathematical model of viscoelastic-plastic deformation of flexible plates cross-reinforced in planes parallel to the middle plane is developed on the basis of the algorithm of time steps. The deformations of the components of the composition of the plates are assumed to be small and they are decomposed into elastic and plastic components. The viscoelastic behavior of the composition materials is subject to the relations of the Maxwell–Boltzmann body. Inelastic deformation is defined by the equations of the theory of plastic flow with isotropic hardening. The normal stresses in the transverse direction are linearly approximated over the thickness of the plates. Therefore, linear deformations in the transverse direction and their velocities are excluded from the governing equations for the composition components. The weakened resistance of fibrous plates to transverse shear is taken into account in the framework of the non-classical Reddy bending theory. The geometric nonlinearity of the problem is considered in the Karman approximation. The formulated initial-boundary value problems are solved numerically using an explicit scheme of the “cross” type. To obtain a stable numerical scheme, an artificial technique is used: the stresses in the Maxwell – Boltzmann viscoelastic relations at the current discrete time are expressed in terms of the stress velocity by the trapezoid formula with a step back. The elastic-plastic and viscoelastic-plastic bending dynamic behavior is investigated for the relatively thick orthogonally reinforced fiberglass rectangular plates under the action of explosive loads. It is shown that a change in the structure of reinforcement leads to a change in the value of the residual deflection of the structure. It was found that the amplitude of oscillations of the reinforced plate in the vicinity of the initial time instant significantly exceeds the value of the residual deflection.
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