柔性圆柱加筋壳热弹粘塑性动态变形建模

Andrei P. YANKOVSKII
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引用次数: 0

摘要

建立了具有复杂配筋结构的薄圆柱壳的热弹粘塑性弯曲动力变形数学模型。在Ambartsumyan的非经典弯曲理论框架下,对这种复合结构的横向剪切和波浪过程的弱阻力进行了建模。在卡门近似中考虑了问题的几何非线性。所述组合材料各向同性;它们的塑性变形用流动理论与依赖于温度和应变速率的加载函数的关系来描述。考虑到所考虑的问题的热力和机械组成部分之间的联系。在结构的横向上,温度近似为7阶多项式。采用显式时间步长格式,对公式化的非线性二维初边值问题进行了数值积分。研究了经纵向和周向正交加固的玻璃纤维和金属复合材料长圆柱壳的弹粘塑性和弹塑性动力性能。结构从内部加载压力,这类似于空气冲击波中的压力。结果表明,在轴对称变形过程中,柔性玻璃纤维壳在某些点上可承受11 ~ 13℃的额外加热。几何形状相似的金属复合结构和加固结构-温度降低40…60°C。与热弹粘塑性计算相比,热弹塑性计算导致玻璃纤维外壳的最高温限值高估了1.0 ~ 1.5°C,而对于金属复合材料结构,相反,这些值低估了20°C。结果表明,玻璃纤维壳的计算可以不考虑其内部的热响应,而金属复合材料壳的动力学计算可以考虑其内部的温度响应。在计算金属复合材料和玻璃纤维结构的动力性能时,必须考虑其组成成分的塑性性能对应变速率的敏感性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
MODELING OF THERMOELASTIC-VISCOPLASTIC DYNAMIC DEFORMATION OF FLEXIBLE CYLINDRICAL REINFORCED SHELLS
A mathematical model of thermoelastic-viscoplastic flexural dynamic deformation of thin circular cylindrical shells with complex reinforcement structures is developed. Weak resistance to transverse shear and wave processes in such composite structures are modeled in the framework of Ambartsumyan’s non-classical theory of bending. The geometric nonlinearity of the problem is taken into account in the Karman approximation. The composition materials are isotropic; their plastic deformation is described by the relations of the flow theory with a loading function that depends on temperature and strain rate. The connection between the thermal and mechanical components of the problem under consideration is taken into account. In the transverse direction of structures, the temperature is approximated by a 7th order polynomial. The formulated nonlinear two-dimensional initial-boundary value problem is numerically integrated using an explicit scheme of time steps. The elastic-viscoplastic and elastic-plastic dynamic behavior of fiberglass and metal-composite long cylindrical shells, which are orthogonally reinforced in the circumferential and longitudinal directions, is studied. Structures are loaded from the inside with pressure, which is similar to the pressure in an air blast wave. It is shown that flexible fiberglass shells during axisymmetric deformation can experience additional heating by 11…13 °C at certain points. Metal-composite structures similar in geometry and reinforcement structure — by 40…60 °C. Thermo-elastoplastic calculations lead to an overestimation of the maximum temperature values in fiberglass shells by 1.0…1.5 °C compared to thermoelastic-viscoplastic calculations, and for metal-composite structures, on the contrary, to an underestimation of these values by 20 °C. It is shown that the calculations of fiberglass shells can be carried out without taking into account the thermal response in them, and it is advisable to calculate the dynamics of metal-composite shells, taking into account the temperature response in them. The dynamic behavior of both metal-composite and fiberglass structures must be calculated taking into account the sensitivity of the plastic properties of their composition components to the strain rate.
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