Aviation turbulence is modelled as an interaction between an aircraft and a vortex tube. The vortex tube can have an arbitrary orientation/offset with respect to the aircraft. We compare modelling the aircraft (i) as a point and (ii) having a finite area (wing and fuselage). We consider both vertical and horizontal accelerations experienced by the aircraft. The baseline vortex tube has an area which is of the order of the aircraft area.

中文翻译：

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涡激航空湍流建模

航空湍流被建模为飞机和涡流管之间的相互作用。涡流管可以具有相对于飞行器的任意取向/偏移。我们比较建模飞机 (i) 作为一个点和 (ii) 具有有限区域（机翼和机身）。我们考虑飞机经历的垂直和水平加速度。基线涡流管的面积是飞机面积的数量级。