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

Yi Jiang*, Qi Liu, Xiaolin Zhang

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

3 Citations (Scopus)

Abstract

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.

Original languageEnglish
Pages (from-to)53-55
Number of pages3
JournalBinggong Xuebao/Acta Armamentarii
Volume25
Issue number1
Publication statusPublished - Jan 2004

Keywords

  • Ant-tank missile
  • Calculational fluid dynamics
  • Punching rudder
  • Three-dimensional Navier-Stokes equation

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