弹药技术

无人机机载炸弹投放分离特性数值模拟研究

  • 周培培 ,
  • 郭少杰 ,
  • 王斌 ,
  • 张桂茹
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  • 中国航天空气动力技术研究院,北京100074

周培培(1984-),男,河南南阳人,工程师,研究方向:飞行器设计与计算空气动力学。

收稿日期: 2016-03-03

  网络出版日期: 2025-05-23

Numerical Simulation Study of the Characteristic of Separation of UAV Airborne Bomb Release

  • ZHOU Peipei ,
  • GUO Shaojie ,
  • WANG Bin ,
  • ZHANG Guiru
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  • China Academy of Aerospace Aerodynamics, Beijing 100074, China

Received date: 2016-03-03

  Online published: 2025-05-23

摘要

通过在非结构动态重叠网格上耦合求解刚体六自由度运动方程和非定常N-S方程的方法,对无人机机载炸弹投放分离过程中的气动特性和运动轨迹进行了数值模拟研究,获得了炸弹运动过程中的轨迹、姿态等信息,分析了炸弹投放分离过程中的安全性问题。研究表明,在计算攻角范围内(α=1°、5°),无横风条件下炸弹的投放是安全的;有横风(5m/s、10m/s)条件下炸弹的投放是不安全的。

本文引用格式

周培培 , 郭少杰 , 王斌 , 张桂茹 . 无人机机载炸弹投放分离特性数值模拟研究[J]. 弹箭与制导学报, 2017 , 37(2) : 87 -91 . DOI: 10.15892/j.cnki.djzdxb.2017.02.021

Abstract

By coupling resolving the 6-DOF motion equation of rigid body and unsteady N-S equation on unstructured dynamic overlapping grids, the numerical simulation of aerodynamic characteristics and the trajectory of UAV airborne bomb in the process of release and separation was carried out. The trajectory and attitude of airborne weapon separation in the process of the bomb movement were obtained and the security issues in the process of bomb release and sepration were analyzed. The results showed that in the calculation of angle of attack range (α = 1°、5°), the bomb release was safe without crosswind, while the bomb realease was not safe when under a crosswind( 5 m/s、10 m/s).

参考文献

[1]
MURMAN S M,AFTOSMIS M J,BERGER M J. Simulations of 6-DOF motion with a Cartesian method: AIAA 2003-1246 [R]. 2003.
[2]
HALL LH,PARTHASARATHY V. Validation of an automated Chimera/6-DOF methodology for multiple moving body problems[C]//Proceedings of 36th AIAA Aerospace Sciences Meeting and Exhibit. [S.l.:s.n.],1998.
[3]
NAKAHASHI K,TOGASHI F,SHAROV D. Intergridboundary definition method for overset unstructured grid approach [J]. AIAA Journal,2000,38(11) : 2077-2084.
[4]
TOGASHI F,NAKAHASHI K,ITO Y,et al. Flow simulation of NAL experimental supersonic airplane/booster separation using overset unstructured grids [J]. Computers & Fluids,2001,30(6) : 637-688.
[5]
SICKLES W L,POWER G D,CALAHAN J A,et al. Application of a CFD moving-body system to multicomponent store separation: AIAA 2007-4073 [R]. 2007.
[6]
FREEMAN J A. Applied computational fluid dynamics for aircraft-store design,analysis and compatibility [C]∥Proceedings of 44th Aerospace Sciences Meeting and Exhibit. [S.l.: s.n.],2006.
[7]
周培培,蒋胜矩,李杰. 基于动态嵌套网格的非定常气动力数值模拟[J]. 弹箭与制导学报,2010,30 (5) : 143-146.
[8]
许晓平,周洲,范锐军,等. 基于动态嵌套网格技术的机载武器投放研究[J]. 兵工学报,2010,31 (9) : 1241-1246.
[9]
李孝伟,范绪箕. 基于动态嵌套网格的飞行器外挂物投放的数值模拟[J]. 空气动力学报,2004,22 (1) : 114-117.
[10]
王正裕,李孝伟. 基于动态嵌套网格技术的飞行器导弹发射的数值模拟[J]. 上海大学学报(自然科学版) ,2008,14(2) : 173-176.
[11]
段旭鹏,常兴华,张来平. 基于动态混合网格的多体分离数值模拟方法[J]. 空气动力学学报,2011,29 (4) : 447-452.
[12]
朱冰,杨涓,祝小平. 基于改进模型的察/打无人机武器分离仿真[J]. 西北工业大学学报,2015,33(1) : 21-25.
[13]
朱冰,祝小平,周洲,等. 基于非结构动网格的多体分离数值仿真研究[J]. 空气动力学学报,2013,31 (2) : 181-185.
[14]
唐志共,李彬,郑鸣,等. 飞行器外挂投放数值模拟 [J].空气动力学学报,2009,27(5) : 592-595.
[15]
张辉,谭俊杰,崔东明. 非结构重叠网格方法研究及应用[J]. 计算力学学报,2010,27(1) : 162-168.
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