The exhaust jet in the exhaust channel of the vertical launching system(VLS) during a missile launches was researched using the numerical methods in this paper.

 
  • 采用數值計算方法對導彈在艦載導彈垂直發(fā)射裝置中排導系統內的燃氣流場(chǎng)進(jìn)行了仿真分析,認為導彈垂直起飛過(guò)程中高速燃氣射流可將外部冷空氣引射入排導系統內。
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