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LARGE EDDY SIMULATION OF AIRCRAFT WAKE VORTICES WITHIN HOMOGENEOUS TURBULENCE: CROW INSTABILITY

机译:均质湍流中飞机尾迹涡的大涡模拟:乌鸦不稳定

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摘要

Ambient atmospheric turbulence effects on aircraft wake vortices are studied using a validated large eddy simulation model. Our results confirm that the most amplified wavelength wavelength of the Crow instability and the lifetime of wake vortices are significantly influenced by ambient turbulence (Crow,S.C.,"Stability Theory for a Pair of Trailing Vortices,"AIAA Journal,Vol.8,No.12,1970,pp.2172-2179).The Crow instability becomes well developed in most atmospheric turbulence levels, but in strong turbulence the vortex pair deforms more irregularly due to turbulence advection. The most amplified wavelength of the instability decreases with increasing dimensionless turbulence intensity η ,although it increases with increasing turbulence integral length scale. The vortex lifespan is controlled primarily by η and decreases with increasing η,whereas the effect of integral scale of turbulence on vortex lifespan is of minor importance.
机译:使用已验证的大型涡流仿真模型研究了大气湍流对飞机尾流涡流的影响。我们的结果证实,乌鸦不稳定性的最大放大波长波长和尾流涡旋的寿命受到周围湍流的显着影响(乌鸦,SC,“一对尾涡的稳定性理论”,AIAA杂志,第8卷,第5期)。 12,1970,pp.2172-2179)。在大多数大气湍流水平下,乌鸦的不稳定性都得到了很好的发展,但是在强湍流中,涡流对由于湍流对流而更不规则地变形。不稳定性的最大放大波长随无量纲湍流强度η的增加而减小,尽管随湍流积分长度尺度的增加而增加。涡流寿命主要受η的控制,并随η的增加而减小,而湍流积分尺度对涡流寿命的影响次要。

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