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Mechanism of Generation and Collapse of a Longitudinal Vortex System Induced around the Leading Edge of a Delta Wing

机译:三角翼前缘引起的纵向涡旋系统产生和坍塌的机理

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The purpose of the paper is to clarify the mechanism of generation and collapse of a longitudinal vortex system induced around the leading edge of a delta wing. CFD captured well characteristics of flow structure of the vortex system. It is found that the vortex system has a cone-shaped configuration, and both rotational velocity and vorticity have their largest values at the tip of the vortex and reduce downstream along the vortical axis. This resulted in inducing the largest negative pressure at the tip of the delta wing surface. The collapse of the vortex system was also studied. The system can still remain until the tip angle of 110 degrees. However, between 110 degrees and 120 degrees, the system becomes unstable. Over 120 degrees, the characteristics of the vortex are considered to have converted from the longitudinal vortex to the transverse one.
机译:本文的目的是阐明在三角翼前缘周围引起的纵向涡旋系统产生和坍塌的机理。 CFD捕获了旋涡系统流动结构的井特征。发现涡旋系统具有圆锥形的构造,并且旋转速度和涡度在涡旋的尖端处具有最大值,并且沿着涡旋轴向下游减小。这导致在三角翼表面尖端处引起最大的负压。还研究了涡旋系统的崩溃。该系统仍然可以保持到110度的顶角。但是,在110度和120度之间,系统变得不稳定。在120度以上,涡旋的特性被认为已从纵向涡旋转换为横向涡旋。

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