Numerical Analysis of Refueling Drogue Oscillation During Refueling Docking

被引：0
|
作者：
Chen Lele [1 ]
Liu Xueqiang [1 ]
机构：
[1] College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics
来源：
Transactions of Nanjing University of Aeronautics and Astronautics | 2016年 / 33卷 / 02期
基金：
中央高校基本科研业务费专项资金资助;
关键词：
aerial refueling; numerical simulation; refueling drogue; dynamic grid; refueling docking;
D O I：
10.16356/j.1005-1120.2016.02.173
中图分类号：
V271.494 [];
学科分类号：
082503 ;
摘要：
Refueling docking at different velocities is simulated by using computational fluid dynamics(CFD)method.The Osher scheme and S-A turbulence model are used to solve the compressible Navier-Stokes equations,and the Delaunay mapping dynamic grid method is also employed.All the numerical results show that the velocity of refueling docking is very important for aerial refueling.When the velocity is lower than 3m/s,the refueling drogue will move upward with obvious cycle staggering,while moving upward with slight cycle staggering at the speed of3m/s.The results can be referenced by aerial refueling design.
引用
收藏
页码：173 / 179
页数：7
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