基于对流扩散方程FDTD求解的飞机尾流涡散射特性

Chun Shen, Jianbing Li, Yongzhen Li, XueSong Wang
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引用次数: 2

摘要

飞机尾流涡是航空领域的一种非常严重的危害,雷达对尾流涡的探测是监测尾流涡行为和预测尾流涡演变的一种很好的方法。为了研究尾流的雷达散射特性,本文提出了一个关于水蒸气、位温等被动保守变量的对流扩散方程来描述尾流的动力学。然后利用时域有限差分法对该方程进行求解,得到尾流的时空演化,并以此计算尾流的RCS。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Scattering Characteristics of Aircraft Wake Vortex Based on the FDTD Solution of Convection-Diffusion Equation
Aircraft wake vortex is a very series hazard in aviation, and the radar detection of it could serve as a good solution to monitor its behavior and predict its evolution. To study the radar scattering characteristics, this paper proposes to describe the dynamics of wake vortex with a convection-diffusion equation about some passive conservative variables such as water vapor, potential temperature, etc. Then the FDTD method is employed to solve this equation to get the temporal and spatial evolutions of wake vortex, which are then used to calculate the RCS of wake vortex.
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