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Structure buckling hybrid reliability analysis of a supercavitating projectile using a model with truncated probability and multi-ellipsoid convex set uncertainties

机译:使用截断概率和多椭球凸面设定不确定性的模型结构屈曲混合混合性可靠性分析

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摘要

Structure buckling problems for supercavitating projectiles are often observed in high underwater velocity operating conditions. As a result, it is necessary to perform a structure buckling reliability analysis. It is common that hboxprobabilistic and nonprobabilistic uncertainty information exist simultaneously. Also, it is reasonable that probability distributions of most random variables in engineering are treated as truncated probability distributions. In this paper, a new hybrid model is proposed, which deals with structure performance function with both truncated probability distribution variables and multi-ellipsoid convex set variables. The model discussed here is adapted for two separate cases in the standard super-sphere space, i.e., limit state surface interferences with a unit super-sphere region or not. The hybrid reliability index is calculated using a modified limit step length iteration algorithm to ensure convergence. Good convergence and validity of the iteration algorithm are verified using numerical examples with highly nonlinear structure performance function. The hybrid model is applied to the structure buckling hybrid reliability analysis of a supercavitating projectile. Results show that structure buckling hybrid reliability index increases with the increase in the ratio of base diameter to cavitator diameter, and decreases with the increase of initial launch velocity. Also, uncertainty degree of cavitator drag coefficient and initial launch velocity should be controlled in demonstration for high structure buckling reliability of supercavitating projectiles.
机译:在高水下速度运行条件下通常观察到超级挖掘射弹的结构屈曲问题。结果,有必要执行结构屈曲可靠性分析。很常见的是,同时存在 hboxprobabilistic和非特性不确定性信息。此外,合理的是,工程中最随机变量的概率分布被视为截断概率分布。在本文中,提出了一种新的混合模型,该模型涉及具有截断概率分布变量和多椭ellipsoId凸起集变量的结构性能功能。这里讨论的模型适用于标准超球空间中的两个单独的情况,即限制与单位超球区域的状态表面干扰。使用修改的限制步长迭代算法计算混合可靠性指数以确保收敛。使用具有高度非线性结构性能功能的数值示例来验证迭代算法的良好收敛性和有效性。混合模型应用于超渗透射弹的结构屈曲混合性可靠性分析。结果表明,结构屈曲混合可靠性指数随着基部直径与空穴直径的比率的增加而增加,随着初始发射速度的增加而降低。此外,应在高结构屈曲可靠性的示范中控制空穴阻力系数和初始发射速度的不确定性程度。

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