Analysis of Damage Characteristicsof Missile Rudder Fins Subjected to Projectile Penetration

Yong HE; Zengyou LIANG; Chenyang LIANG; Xiaojian WANG

doi:10.12382/bgxb.2025.0795

您当前的位置：

首页 >

文章列表页 >

Analysis of Damage Characteristicsof Missile Rudder Fins Subjected to Projectile Penetration

更新时间：2026-02-10

- Analysis of Damage Characteristicsof Missile Rudder Fins Subjected to Projectile Penetration
- Acta Armamentarii Vol. 46, Issue S2, Pages: 250795(2025)
- 作者机构：
  
  中北大学机电工程学院, 山西太原 030051
- 作者简介：
- 基金信息：
- DOI：10.12382/bgxb.2025.0795
  CLC：
- Received：01 September 2025，
  
  Online First：03 February 2026，
  
  Published：2025
- 稿件说明：
移动端阅览
Yong HE, Zengyou LIANG, Chenyang LIANG, et al. Analysis of Damage Characteristicsof Missile Rudder Fins Subjected to Projectile Penetration[J]. Acta Armamentarii, 2025, 46(S2): 250795.
DOI：

Yong HE, Zengyou LIANG, Chenyang LIANG, et al. Analysis of Damage Characteristicsof Missile Rudder Fins Subjected to Projectile Penetration[J]. Acta Armamentarii, 2025, 46(S2): 250795. DOI： 10.12382/bgxb.2025.0795.

摘要

为研究弹丸以不同条件侵彻时

舵机翼片的毁伤特性

采用数值模拟的方法

以某导弹舵机翼片为研究对象

模拟受卵形弹弹丸以不同初速和角度侵彻时舵片的毁伤情况

研究了弹丸初速、侵彻角度2种因素对舵片损伤面积和表面凹陷深度的影响。研究表明

在不同弹丸初速和侵彻角度下

舵片的毁伤程度存在很大差异

舵片毁伤模式主要呈现蒙皮变形、穿孔损伤、骨架变形/破坏及大面积撕裂5种典型形式。高速侵彻时

弹丸所造成的损伤面积更大

也更容易贯穿舵片

对舵片的毁伤更严重。在弹丸初速不变时

侵彻角度越大

弹丸侵彻舵片时更易发生跳弹现象

从而形成破坏程度越低的损伤。但值得注意的是

当弹丸初速较高时

大角度的侵彻会使舵片产生大面积的撕裂损伤

形成严重的破坏。

Abstract

The damage characteristics of missile rudder fins subjected to projectile penetration under varying conditions are studied.The damage characteristics of a typical missile rudder fin penetrated by an ogive-nose projectile at different striking velocities and impact angles are numerically simulated.The effects of projectile initial velocity and penetration angle on the damage area and surface indentation depth of rudder fins are systematically analyzed.Results demonstrate that the degrees of damage of rudder fins under the different initial velocities and penetration angles of projectile significantly vary.Five characteristic failure modes of rudder fins

i.e.

skin deformation

perforation damage

frame deformation

frame fracture and large-area tearing.are identified.High-velocity penetration induces larger damage areas and higher perforation propensity

leading to more severe structural compromise.At constant projectile initial velocity

the increased penetration angles promote ricochet phenomena

thereby reducing the damage severity.Notably

under high-velocity conditions

the steep impact angles trigger an extensive tearing damage via projectile deflection and material extrusion

resulting in catastrophic failure.

关键词

Keywords

references

王伟 , 张宏岩 , 刘佳琪 , 等 . 俄乌冲突对陆战制导弹药发展的影响研究 [J ] . 战术导弹技术 , 2024 ( 1 ): 150 - 160 .

WANG W , ZHANG H Y , LIU J Q , et al. Research on the influence of the Russia-Ukraine conflict on the development of land combat guided munitions [J ] . Tactical Missile Technology , 2024 ( 1 ): 150 - 160 . (in Chinese)

王雅琳 , 张灿 , 宋怡然 , 等 . 世界飞航导弹武器装备与技术近5年发展回顾与展望 [J ] . 战术导弹技术 , 2020 ,( 4 ): 71 - 78 ,143.

WANG Y L , ZHANG C , SONG Y R , et al. Reviews and outlooks of global aerodynamic missiles evolution in 5 years version [J ] . Tactical Missile Technology , 2020 ,( 4 ): 71 - 78 ,143. (in Chinese)

ZHENG S C , FU Y L , WANG D Y , et al. Investigations on system integration method and dynamic performance of electromechanical actuator [J ] . Science Progress , 2020 , 103 ( 3 ): 0036850420940923 .

郭庆亮 , 徐敏 , 姚伟刚 , 等 . 导弹异形卷弧翼安装选型 [J ] . 计算机辅助工程 , 2010 , 19 ( 2 ): 60 - 63 .

GUO Q L , XU M , YAO W G , et al. Selection and installation of abnormity wrap around fins of missile [J ] . Computer Aided Engineering , 2010 , 19 ( 2 ): 60 - 63 . (in Chinese)

田晓丽 , 陈国光 . 高速大长径比火箭弹动态特性分析 [J ] . 华北工学院学报 , 2001 ( 6 ): 402 - 406 .

TIAN X L , CHEN G G . The dynamic characteristics analysis of high speed slender rocket [J ] . Journal of North China Institute of Technology , 2001 ( 6 ): 402 - 406 .

IRWIN A J , RENDER P M . The influence of mid-chord battle damage on the aerodynamic characteristics of two-dimensional wings [J ] . The Aeronautical Journal , 2000 , 104 ( 1033 ): 153 - 161 .

SHAH G . Aerodynamic effects and modeling of damage to transport aircraft [C ] // AIAA atmospheric flight mechanics conference and exhibit . 2008 : 6203 .

AHN J M , KIM K , SUK J . Dynamic analysis of an asymmetric UAV with partial wing damage [C ] // 2011 11th International Conference on Control,Automation and Systems.IEEE , 2011 : 112 - 116 .

廖贵超 . 爆炸冲击波对小型导弹目标的破坏性分析 [D ] . 南京 : 南京理工大学 , 2013 .

LIAO G C . Damage analysis of explosive shock waves on small missiletargets [D ] . Nanjing : Nanjing University of Science and Technology , 2013 . (in Chinese)

刘断尘 . 舵机折叠舵展开性能分析及试验 [D ] . 长春 : 中国科学院研究生院(长春光学精密机械与物理研究所) , 2015 .

LIU D C . Deployment performance analysis and testing of servo-actuated foldingrudders [D ] . Changchun : Graduate University of Chinese Academy of Sciences (Changchun Institute of Optics,Fine Mechanics and Physics), 2015 . (in Chinese)

高玉伟 , 韩庆 , 张锋 , 等 . 作战飞机翼面损伤对其气动特性的影响研究 [J ] . 飞行力学 , 2013 , 31 ( 5 ): 394 - 397 .

GAO Y W , HAN Q , ZHANG F , et al. Influence of combat aircraft’s wing surface damaged on longitudinal aerodynamic characteristics [J ] . Flight Dynamics , 2013 , 31 ( 5 ): 394 - 397 . (in Chinese)

高宗战 , 王毅 , 黄帅军 , 等 . 导弹舵面的复合材料设计与分析 [J ] . 航空兵器 , 2016 ,( 4 ): 63 - 68 .

GAO Z Z , WANG Y , HUANG S J , et al. Design and analysis of composite material for missile rudder [J ] . Aero Weaponry , 2016 ,( 4 ): 63 - 68 . (in Chinese)

贺欢 . 基于弹目交会的坦克主动防御技术研究 [D ] . 太原 : 中北大学 , 2024 .

HE H . Research on tank active protection technology based on projectile-target encounter [D ] . Taiyuan : North University of China , 2024 . (in Chinese)

FAUZI M N A , UDAY M B , ZUHAILAWATI H , et al. Microstructure and mechanical properties of alumina-6061 aluminum alloy joined by friction welding [J ] . Materials & Design , 2010 , 31 ( 2 ): 670 - 676 .

OUIBRAHIM A , DJELLAL S . Experimental Investigation on Aerodynamic Performance of Damaged Wings [C ] // Proceedings of the 5th European & African Conference on Wind Engineering.Florence , Italy : Firenze University Press , 2009 : 1000 - 1002 .

侯云锟 , 唐奎 , 王金相 , 等 . 不同弹头夹心弹斜侵彻金属靶特性 [J ] . 兵工学报 , 2025 , 46 ( 4 ): 215 - 229 .

HOU Y K , TANG K , WANG J X , et al. Characteristics of oblique penetration ofmetal targets by jacketed rods with different noses [J ] . Acta Armamentarii , 2025 , 46 ( 4 ): 215 - 229 . (in Chinese)

LIU Z S , SWADDIWUDHIPONG S , ISLAM M J . Perforation of steel and aluminum targets using a modified Johnson-Cook materialmodel [J ] . Nuclear Engineering and Design , 2012 , 250 : 108 - 115 .

余双洋 , 彭永 . 4340钢弹侵彻45号钢靶的温升数值模拟 [J ] . 兵工学报 , 2023 , 44 ( 增刊1 ): 144 - 151 .

YU S Y , PENG Y . Numerical simulation of temperature rise of 4340 steel projectile penetrating into 45# steel target [J ] . Acta Armamentarii , 2023 , 44 ( S1 ): 144 - 151 . (in Chinese)

TARVER C M , MCGUIRE E M . Reactive flow modeling of the interaction of TATB detonation waves with inert materials [R ] . Livermore,CA , US : Lawrence Livermore National Lab , 2002 .

沈文锦 . 6061铝合金本构模型构建与断裂准则研究 [D ] . 太原 : 太原理工大学 , 2024 .

SHEN W J . Construction of constitutive model and research on fracture criterion for 6061 aluminumalloy [D ] . Taiyuan : Taiyuan University of Technology , 2024 . (in Chinese)

陈刚 , 陈小伟 , 陈忠富 , 等 . A3钢钝头弹撞击45钢板破坏模式的数值分析 [J ] . 爆炸与冲击 , 2007 , 27 ( 5 ): 390 - 397 .

CHEN G , CHEN X W , CHEN Z F , et al. Simulations of A3 steel blunt projectiles impacting 45 steel plates [J ] . Explosion and Shock Waves , 2007 , 27 ( 5 ): 390 - 397 . (in Chinese)

Views

下载量

CNKI被引量

Alert me when the article has been cited

提交

Tools

Publicity Resources

Simulation Analysis of Projectile Penetrating into Rock-like Targets based on Eulerian Algorithm

Numerical Simulation of Temperature Rise of 4340 Steel Projectile Penetrating into 45# Steel Target

Numerical Simulation of Bullets Penetrating into Gelatin Target with Hard/Soft Composite Armor

Numerical Simulation and Experimental Research on Integral Multiple Explosively Formed Projectile Warhead

Simulative Analysis and Experimental Test of Composite Fragile Projectile Under Impact Dynamics

Related Author

Hao SUN

Fengtao BAI

Hang YAO

Bingwen QIAN

Shuangyang YU

Yong PENG

LUO Shao-min

XU Cheng

Related Institution

School of Engineering,Ocean University of China

Northwest Institute of Nuclear Technology

College of Science, National University of Defense Technology

School of Mechanical Engineering，Nanjing University of Science and Technology

School of Science, Nanjing University of Science and Technology

Postal code：100089
Tel：010-68963060/68962718 Fax：010-68963025 Email：bgxb@cos.org.cn
Technical support is provided by Beijing Founder electronics co., LTD 京ICP备05059581号-4 京公网安备11010802024360号
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.
Total Visits：49231 Visits Today：28

⁰