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Stress relaxation in composite flywheels

机译:复合飞轮中的应力松弛

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摘要

A viscoelastic analysis has been developed to investigate stress relaxation and creep in a multi-layered composite cylinder subjected to rotation. The analysis accounts for ply-by-ply variation of material properties, fiber orientations, and density gradients through the thickness of cylinders. A closed form solution based on the corresponding elastic problem is derived for a generalized plane strain state in a thick-walled multi-layered cylinder. Laplace transform is then applied to obtain the numerical solution of the viscoelastic problem. The paper illustrates the derivation of the analytical model and solution procedure. A numerical simulation shows substantial creep and stress relaxation in thick-walled cylinders at an elevated temperature. Viscoelastic effects of composite can result in a drastic change of stress and strain profiles in a cylinder over a period of time, which is critical in terms of structural durability for application such as energy storage flywheels.
机译:已经开发了一种粘弹性分析来研究对经受旋转的多层复合圆筒的应力松弛和蠕变。通过圆柱体的厚度,分析占材料特性,纤维方向和密度梯度的底层变化。基于相应的弹性问题的封闭形式溶液在厚壁的多层圆柱体中的广义平面应变状态导出。然后施加拉普拉斯变换以获得粘弹性问题的数值溶液。本文说明了分析模型和解决方案程序的推导。数值模拟在升高的温度下显示厚壁圆柱体中的大量蠕变和应力松弛。复合材料的粘弹性效果可以在一段时间内圆柱体中的应力和应变型材的急剧变化,这对于诸如储能飞轮的应用的结构耐久性方面至关重要。

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