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滑翔增程弹气动特性分析
引用本文:武频,赵润祥,谭俊杰,郭锡福. 滑翔增程弹气动特性分析[J]. 弹道学报, 2001, 13(4): 38-41
作者姓名:武频  赵润祥  谭俊杰  郭锡福
作者单位:南京理工大学动力工程学院,
摘    要:针对滑翔增程弹在有弹翼和无机翼两种情况下,气动特性进行了计算、分析和比较。计算结果表明,有弹翼时滑翔增程弹的升阻比与无弹翼时的升阻比相比大得多,因此滑翔增程弹能够较好的达到滑翔增程的目的。

关 键 词:滑翔增程弹 弹翼 气动特性 射程 开阻比
修稿时间:2001-04-23

THE ANALYSIS OF AERODYNAMIC CHARACTER ON GLIDE BULLET TO INCREASE RANGE
Wu Pin Zhao Runxiang Tan Junjie Guo Xifu. THE ANALYSIS OF AERODYNAMIC CHARACTER ON GLIDE BULLET TO INCREASE RANGE[J]. Journal of Ballistics, 2001, 13(4): 38-41
Authors:Wu Pin Zhao Runxiang Tan Junjie Guo Xifu
Abstract:This paper mainly calculated, analyzed and compared two kinds of glide bullets, one has wing, and the other has no wing. The calculated results indicate that the lift force of the glide bullet which has wing is much bigger than that has no wing, and it reached the aim to increase range.
Keywords:glide bullet   wing   aerodynamic character   range
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