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Methodologies of stochastic simulation for helicopter accidents and nonparametric evaluation of the stochastic responses

机译:直升机事故随机模拟方法和随机响应的非参数评估

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The paper aims to develop stochastic simulation and nonparametric analysis methods for investigation into and harm minimisation of helicopter accidents resulting from a total engine failure. An innovative, stochastic simulation scheme is established for investigating the variability in a full crash event by incorporating the methodologies of hierarchical stochastic simulation and nonparametric analysis. By employing Monte Carlo algorithms in flight emergency and structure crash simulations, a stochastic simulation method is developed for establishing robust correlations between the critical parameters prior to helicopter accidents and possible occupant injury metrics. Based on the nonparametric analysis performed on the stochastic injury responses, a solution is proposed to predict and evaluate the potential severity of occupant's injuries resulting from this class of helicopter accidents. A comparison of using the nonparametric strategy into three different thicknesses of subfloor tubes develops the potential for evaluating the stochastic injury results of the helicopter accidents.
机译:本文旨在开发随机模拟和非参数分析方法,以调查和最大程度降低因发动机整体故障而导致的直升机事故的危害。建立了一种创新的随机仿真方案,通过结合分层随机仿真和非参数分析的方法来研究完全碰撞事件中的可变性。通过在飞行紧急情况和结构碰撞模拟中采用蒙特卡洛算法,开发了一种随机模拟方法,用于在直升机事故之前的关键参数与可能的乘员伤害度量之间建立稳固的相关性。基于对随机伤害响应进行的非参数分析,提出了一种解决方案,以预测和评估此类直升机事故造成的乘员潜在伤害严重程度。将非参数策略用于三种不同厚度的底层地板管的比较,为评估直升机事故的随机伤害结果提供了潜力。

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