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Development of a temporal evolution model for aero-optical effects caused by vortices in the supersonic mixing layer

机译:超音速混合层中由涡旋引起的航空光学效应的时间演化模型的建立

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摘要

The vortices inside mixing layers impose remarkable aero-optical distortions on a beam even at moderate subsonic speeds. Knowledge about aero-optical effects caused by vortices in the flow field, especially their spatial and temporal evolution, is limited for supersonic mixing layers because the flows have very high speeds. In this paper, the temporal evolution of aero-optical effects caused by vortices in the supersonic mixing layer was investigated. A large eddy simulation was used to simulate the supersonic flow. A novel approach, coordinate extraction of vortex core, which is based on the relationship between vortices and the profile of the optical path length over the flow field, was proposed to quantitatively calculate the radii and convective speeds of vortices. A model used to quantitatively describe the temporal evolution of aero-optical effects caused by vortices in the supersonic mixing layer was developed and validated with data of numerical calculation. The results indicated that the model is available. Finally, several conclusions drawn from this work were presented. (C) 2016 Optical Society of America
机译:即使在中等亚音速下,混合层内部的涡流也会使光束产生明显的航空光学畸变。对于超音速混合层,关于由流场中的涡流引起的航空光学效应(尤其是其时空演化)的知识是有限的,因为这些流具有非常高的速度。本文研究了超声速混合层中由涡旋引起的航空光学效应的时间演化。大涡模拟被用来模拟超音速流动。提出了一种新的方法,即涡流的坐标提取,该方法基于涡流与流场上光程长度的分布之间的关系,定量地计算了涡流的半径和对流速度。建立了用于定量描述超音速混合层中涡流引起的航空光学效应随时间变化的模型,并用数值计算数据进行了验证。结果表明该模型可用。最后,提出了从这项工作中得出的一些结论。 (C)2016美国眼镜学会

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