Vortex Wake behind an Aircraft with a High-Aspect-Ratio Wing

被引：1
作者：
Gaifullin, A. M. [1 ]
机构：
[1] Zhukovskii Cent Aerohydrodynam Inst TsAGI, Zhukovskii 140181, Moscow Oblast, Russia
来源：
FLUID DYNAMICS | 2023年 / 58卷 / SUPPL 1期
关键词：
aircraft; vortex wake; atmospheric turbulence; Crow instability; vortex-wake instability; DECAY; VORTICES; MODEL;
D O I：
10.1134/S0015462823600426
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
The problem of determining the characteristics of the vortex wake behind aircraft from the moment of its formation to the moment of destruction is considered. The problem is divided into several related subproblems such as flow near an aircraft, vortex-wake evolution and diffusion, and instability and increasing perturbations in the wake. The results of theoretical and computational studies are compared with the experimental data available from publications. The characteristics of vortex wakes are calculated for specific aircraft.
引用
收藏
页码：S153 / S188
页数：36
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