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 |
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页(从-至) | 53-55 |
页数 | 3 |
期刊 | Binggong Xuebao/Acta Armamentarii |
卷 | 25 |
期 | 1 |
出版状态 | 已出版 - 1月 2004 |