首页> 外文会议>8th International Conference on Fibre Reinforced Composites, Sep 13-15, 2000, University of Newcastle, UK >DAMAGE EVOLUTION AND STIFFNESS DEGRADATION OF THICK WALLED FILAMENT WOUND COMPOSITE PIPES SUBJECTED TO INTERNAL PRESSURE AND AXIAL LOAD
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DAMAGE EVOLUTION AND STIFFNESS DEGRADATION OF THICK WALLED FILAMENT WOUND COMPOSITE PIPES SUBJECTED TO INTERNAL PRESSURE AND AXIAL LOAD

机译:承受内部压力和轴向载荷的厚壁缠绕纤维复合材料管的损伤演化和刚度退化

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Thick walled composite pipes loaded beyond first ply failure will show a variation in transverse crack density through the wall thickness. Even in pipes showing global material homogeneity this is likely to occur simply because of the inhomogeneous state of stress through the thickness. In this case, the onset of damage would be at the inner surface. In hybrid composite pipes or pipes with different winding angles, the onset of damage is less predicable, depending on material properties and load condition. In all cases, the loading path could be crucial. In order to get the elastic solution for all kinds of linear elastic materials, lay-ups and load conditions, a finite difference model was used. This method gives a very precise solution of the elastic problem in all radial positions. The 3-dimensional stiffness degradation due to transverse matrix cracking was solved using solutions from a proposed displacement model assuming equally spaced cracks in angle ply structures. The model shows good agreement with finite element results and thin walled pipe experiments. The stress and strain fields of the cracked structure are used with suitable failure criterions for introducing new cracks. From the onset of failure the problem was solved using small load steps to insure all layers to be in consistent state of damage during loading. The general finite difference model applies to all kinds of materials and lay ups. On the other hand, the degradation model is restricted to angle ply regions. Further more, the elastic properties of these regions must be reducible to globally orthotropic material upon homogenisation, with axes coinciding with the global cylindrical co-ordinate system.
机译:超过第一层破坏的厚壁复合管将显示出贯穿壁厚的横向裂纹密度变化。即使在显示整体材料均匀性的管道中,也可能仅由于整个厚度方向上应力的不均匀状态而发生这种情况。在这种情况下,损坏的开始将在内表面。在混合复合管或具有不同缠绕角度的管中,取决于材料特性和负载条件,损坏的发生难以预测。在所有情况下,加载路径都至关重要。为了获得各种线性弹性材料,叠层和载荷条件的弹性解,使用了有限差分模型。该方法可以非常精确地解决所有径向位置的弹性问题。通过使用提出的位移模型的解决方案解决了由于横向基体开裂引起的3维刚度降低,假设角层板结构中的裂缝间距相等。该模型与有限元结果和薄壁管道实验显示出良好的一致性。裂纹结构的应力和应变场与引入新裂纹的合适破坏准则一起使用。从发生故障开始,使用较小的加载步骤解决了问题,以确保所有层在加载过程中始终处于损坏状态。一般的有限差分模型适用于各种材料和叠层。另一方面,退化模型仅限于角度帘布层区域。此外,这些区域的弹性必须在均匀化后对于整体正交异性材料是可还原的,其轴必须与整体圆柱坐标系重合。

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