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Reliability-based knockdown factors for composite cylindrical shells under axial compression

机译:复合材料圆柱壳在轴向压缩下的基于可靠性的分解因子

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摘要

A collection of all available literature data upon experiments of composite cylinders under axial compression is performed. Theoretical estimation of bifurcation load for all the tested cylinders is achieved solving stability differential equations with the use of a combined "bi-modal and torsion" solution and Galerkin approximation. Experimental knockdown factors with respect to theoretical predictions are derived and they are used to tune the imperfection amplitude of an in-house code, which computes collapse load of imperfect cylindrical composite shells using an axy-symmetric sine-shaped imperfection. "Equivalent imperfection amplitudes" are statistically analysed and with the help of imperfections sensitivity curves, Monte Carlo simulations are performed in order to obtain new reliability-based knockdown factor for cylinders with different stacking sequences. The values obtained directly by statistical analysis of the tests results and the ones derived by the statistical analysis of the calibrated imperfection amplitudes represent an improvement with respect to old design values extrapolated from isotropic shells.
机译:对复合材料圆柱体在轴向压缩条件下进行的实验收集了所有可用的文献数据。通过结合使用“双模态和扭转”解和Galerkin近似解,可以求解稳定性微分方程,从而获得了所有测试气缸的分叉载荷的理论估计值。推导了相对于理论预测的实验击倒因子,并将其用于调整内部代码的不完整幅度,该内部代码使用轴对称正弦形不完整来计算不完整圆柱复合材料壳的坍塌载荷。对“等效缺陷幅度”进行统计分析,并借助缺陷灵敏度曲线,进行蒙特卡洛模拟,以便为具有不同堆叠顺序的气缸获取新的基于可靠性的组合系数。通过对测试结果进行统计分析而直接获得的值,以及通过对校准缺陷幅度进行统计分析而得出的值,相对于从各向同性壳体外推的旧设计值而言,代表了一种改进。

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