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Bending of Delaminated Composite Conoidal Shells under Uniformly Distributed Load

机译:均布载荷作用下分层复合锥壳的弯曲

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摘要

Conoidal shells are very popular roofing units owing to their aesthetic elegance and stiffness. Many parts of the globe, which were earlier assumed to be seismologically stable, are now being considered as earthquake prone. Hence the necessity to build light structures using composites has become very important. In this paper an eight-noded isoparametric shell element is applied for analyzing the bending behavior of delaminated composite conoidal shells under a uniformly distributed load with different practical boundary conditions. To ensure compatibility of deformation and equilibrium of forces and moments at the delamination crack front, a multipoint constraint algorithm is incorporated, which leads to an unsymmetrical stiffness matrix. This formulation is validated through the solution of benchmark problems. Lamination, curvature, and extent of delamination area are varied to compare the performances of delaminated conoidal shells against those with no damage. The results are carefully observed, and a set of conclusions is presented at the end of the paper.
机译:圆锥形外壳由于其美学优雅和刚度而非常受欢迎。以前被认为是地震稳定的全球许多地区,现在都被认为容易发生地震。因此,使用复合材料建造轻型结构的必要性变得非常重要。本文采用八节点等参壳单元来分析分层复合圆锥壳在均匀分布载荷和不同实际边界条件下的弯曲行为。为了确保变形的兼容性以及分层裂纹前沿处力和力矩的平衡,并入了多点约束算法,这导致了不对称刚度矩阵。通过解决基准问题可以验证此公式。改变叠层,曲率和分层范围,以比较分层的锥壳与未损坏的壳的性能。仔细观察结果,并在本文末尾提供一组结论。

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