Preliminary Analysis of the Glide Extended Range Mechanism of the Extreme Extended Range Projectile

谭献忠; 丁则胜; 陈少松; 徐琴

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Preliminary Analysis of the Glide Extended Range Mechanism of the Extreme Extended Range Projectile

更新时间：2026-09-14

- Preliminary Analysis of the Glide Extended Range Mechanism of the Extreme Extended Range Projectile
- 超远程炮弹滑翔增程机理初步分析
- Vol. 34, Issue 4, Pages: 398-402(2013)
- 作者机构：
  
  南京理工大学能源与动力工程学院
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2013
- 稿件说明：
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谭献忠, 丁则胜, 陈少松, et al. Preliminary Analysis of the Glide Extended Range Mechanism of the Extreme Extended Range Projectile[J]. 2013, 34(4): 398-402.
DOI：

谭献忠, 丁则胜, 陈少松, et al. Preliminary Analysis of the Glide Extended Range Mechanism of the Extreme Extended Range Projectile[J]. 2013, 34(4): 398-402. DOI：

摘要

超远程炮弹采用滑翔增程和先进的简易制导技术

是一种新型的炮弹

对其增程机理进行深入的分析研究有利于达到最佳的增程效果.本文从炮弹滑翔飞行受力分析阐述了滑翔增程机理

并对其气动特性、弹道设计及控制参数设计的主要影响参数进行了分析.初步分析认为:为了得到最佳的滑翔增程效果

炮弹需要具有特殊的气动外形和气动特性

努力提高滑翔炮弹的升阻比;起始滑翔弹道和起始滑翔速度要高

选择起始滑翔时刻在弹道顶点附近有利于增加飞行距离;飞行控制参数进行合理匹配;一般采用最大升阻比法滑翔飞行方式

其滑翔飞行距离较远.

Abstract

Extreme extended range projectile adopted glide extended range technique and advanced simple guidance technology was a new type of projectile.It was in favor of attaining best range-extended effect to analyze and research extended range mechanism of extreme extended range projectile.The glide extended range mechanism was elaborated from the force analysis in glide flight

and the mainly influence parameters on aerodynamic characteristic

trajectory design and control parameter design were analysed.Preliminary analysis shows that

in order to obtain best glide extended range effect

the projectile has a specific aerodynamic shape and aerodynamic characteristic

make great efforts to improve the lift-drag ratio

has a high start glide trajectory and start glide velocity

select start glide time near the peak of the trajectory in favour of increasing flight distance

reasonably match flight control parameter

and generally adopt the glide flight way of maximum lift-drag ratio to obtain long glide flight distance.

关键词

Keywords

references

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