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Numerical Prediction of a Critical Altitude on Electrodynamic Aerobraking in a Hypersonic Continuum-Rarefied Transitional Regime

机译:高亢稀土过渡性能中电动气球临界高度的数值预测

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The electrodynamic aerobraking in atmospheric earth entries is simulated using a computational fluid dynamics analysis to predict the magnetic interaction parameter Q and electrodynamic force at high altitudes H≥70-100 km. As a result, Q is found to be much larger than 1 in altitudes lower than 92 km. In accordance with these large Q, the large electrodynamic force generates at H ≤ 84 km. However, the electrodynamic force suddenly vanishes at H≥86 km in spite of Q》1. Accordingly, the electrodynamic aerobraking is found to have a critical altitude at which the electrodynamic force suddenly vanishes. A time-accurate computation is performed to clarify the mechanism of this sudden change at the critical altitude. The computation reveals that the cause originates from two mechanisms in rarefied flows with a strong Hall effect at high altitudes. The first mechanism is initial Joule heating which occurs at a shock front and is required to initiate an electrodynamic shock layer enlargement. The second is the avalanche ionization inside the shock layer which is triggered by the thermal equilibrium process progressing with the electrodynamic shock layer enlargement.
机译:使用计算流体动力学分析模拟大气接地条目中的电动气动,以预测高海拔H≥70-100公里的磁相互作用参数Q和电动力。因此,Q被发现在低于92公里的海拔高度中大于1。根据这些大Q,大的电动力在H≤84mm处产生。然而,尽管Q“1,电动力突然在H≥86公里处消失。因此,发现电动力充气机具有临界高度,电动力突然消失。执行时间准确的计算以阐明临界高度的这种突然变化的机制。该计算揭示了原因源自稀土流动中的两种机制,高海拔地区的强烈霍尔效应。第一机构是初始焦耳加热,其发生在冲击前部,并且需要启动电动冲击层扩大。第二是在冲击层内部的雪崩电离,其被通过电动冲击层扩大的热平衡过程触发。

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