非定常二维飞机尾流涡的三维可视化

K. Ma, Z. Zheng
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引用次数: 24

摘要

在飞机翼尖周围流动的空气形成水平的类似龙卷风的涡流,这对后面的飞机来说是危险的。这种涡旋的动力学,包括地面和大气的影响,可以通过数值模拟来预测,从而提高机场的安全性和容量。我们介绍了三维技术的可视化时间依赖,二维尾流计算,并在地面附近的这种涡的危险强度。我们描述了一种涡旋核跟踪算法和局部平铺法来可视化涡旋演化。平铺法将随时间变化的二维涡芯转换为三维涡管。最后,采用了一种新颖的方法来计算旋涡管附近区域内每个网格点上的诱导滚转力矩,从而实现了旋涡危险强度的三维可视化
本文章由计算机程序翻译,如有差异,请以英文原文为准。
3D visualization of unsteady 2D airplane wake vortices
Air flowing around the wing tips of an airplane forms horizontal tornado-like vortices that can be dangerous to following aircraft. The dynamics of such vortices, including ground and atmospheric effects, can be predicted by numerical simulation, allowing the safety and capacity of airports to be improved. We introduce three-dimensional techniques for visualizing time-dependent, two-dimensional wake vortex computations, and the hazard strength of such vortices near the ground. We describe a vortex core tracing algorithm and a local tiling method to visualize the vortex evolution. The tiling method converts time-dependent, two-dimensional vortex cores into three-dimensional vortex tubes. Finally, a novel approach is used to calculate the induced rolling moment on the following airplane at each grid point within a region near the vortex tubes and thus allows three-dimensional visualization of the hazard strength of the vortices.<>
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