Digital simulation of pressure on a rudder along with the velocity of a missile

Yi Jiang*, Qi Liu, Xiaolin Zhang

*此作品的通讯作者

科研成果: 期刊稿件文章同行评审

3 引用 (Scopus)

摘要

In order to secure a highpressure source for the operation of the rudder, a punching rudder is generally used in anti-tank missiles. Its key characteristics are that the flow velocity is used of to produce a high pressure for rudder operation when an anti-tank missile is flying. Because the velocity varies in the flight of an anti-tank missile, the pressure in the pump of the rudder is also changing. It is of significance to calculate the pressure in the design of rudders or anti-tank missiles. A method of calculating three-dimensional Navier-Stokes equations was presented. The appropriate range of velocity of anti-tank missile flight was discussed.

源语言英语
页(从-至)53-55
页数3
期刊Binggong Xuebao/Acta Armamentarii
25
1
出版状态已出版 - 1月 2004

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