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A Multiphysics Simulation Approach for Efficient Modeling of Lightning Strike Tests on Aircraft Structures

机译:飞机结构雷击试验有效建模的多物理场仿真方法

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摘要

A numerical approach is proposed and demonstrated for efficient modelling of the thermal plasma behaviour present during a lightning strike event. The approach focuses on events with time-scales from microseconds to milliseconds and combines the finite element method, Magnetohydrodynamics and Similitude theory. Similitude theory is used to scale the problem to require considerably less computing resource. To further reduce the computational burden and to resolve the numerical difficulty of simulating the nearly zero electrical conductivity of air at room temperature an approach based on cold field electron emissions is introduced. Simulations considering turbulent flow have been considered, modelling a test configuration from literature designed to inspect composite material performance and applying an aerospace standard test profile (waveform-B). Predicted peak temperatures (of the order of ~40,000 K) and pressures (of the order of 0.1-0.2 MPa) suggest that the pressure loading during a waveform-B event will have a minimal effect on composite material damage.
机译:提出并证明了一种数值方法,用于对雷击事件期间存在的热等离子体行为进行有效建模。该方法关注时间范围从微秒到毫秒的事件,并结合了有限元方法,磁流体动力学和相似性理论。相似性理论用于解决问题,以减少所需的计算资源。为了进一步减轻计算负担并解决在室温下模拟空气几乎为零的电导率的数值难题,提出了一种基于冷场电子发射的方法。已经考虑了考虑湍流的模拟,根据旨在检查复合材料性能的文献对测试配置进行建模,并应用航空航天标准测试曲线(波形B)。预测的峰值温度(约40,000 K)和压力(约0.1-0.2 MPa)表明,在波形B事件中,压力负载对复合材料的损坏影响最小。

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