弹道与气动力技术

一种基于数值虚拟飞行技术的弹丸稳定性评估方法

  • 蒋胜矩 ,
  • 梁益铭
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  • 中国兵器工业第203研究所,西安 710065

蒋胜矩(1979-),男,河南睢县人,硕士研究生,研究方向:气动布局设计与应用计算流体力学研究。

收稿日期: 2016-04-21

  网络出版日期: 2025-05-23

A Estimation Method for Projectile Stability Based on Numerical Virtual Flight Technology

  • JIANG Shengju ,
  • LIANG Yiming
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  • No. 203 Research Institute of China Ordnance Industries, Xi'an 710065, China

Received date: 2016-04-21

  Online published: 2025-05-23

摘要

基于数值虚拟飞行技术,采用动态嵌套网格,耦合求解非定常N-S方程和六自由度刚体运动方程,发展了一种能够考虑非定常气动效应的弹丸稳定性评估方法。通过对典型外挂物投放标模和BRL的M852子弹标模进行数值模拟,验证了数值方法正确、有效,可以用于数值虚拟飞行模拟。最后对某质量模拟弹丸进行了虚拟飞行模拟,给出了不同扰动情况下的落点散布和飞行稳定性评估结论。

本文引用格式

蒋胜矩 , 梁益铭 . 一种基于数值虚拟飞行技术的弹丸稳定性评估方法[J]. 弹箭与制导学报, 2017 , 37(1) : 121 -124,128 . DOI: 10.15892/j.cnki.djzdxb.2017.01.028

Abstract

Based on numerical virtual flight technology, unsteady N-S equations and 6 DOF equation of motion were coupling soluted using moving chimera grid. A method was developed to estimate projectile stability, and it could consider the effect of unsteady aerodynamic characteristics. Through the numerical simulation of the slandard model for a typical external store release and the standard model of M852 bullet of BRL. The results showed that the numerical method was accurate and available, and it could be used in numerical virtual flight simulation. Finally, the virtual flight simulation of a mass simulated projectile was carried out, and the numerical result gave dispersion and flight stability assessment conclusion under different disturbances.

参考文献

[1]
李浩,赵忠良,范召林. 风洞虚拟飞行试验模拟方法研究[J]. 实验流体力学,2011,25(6) : 72-76.
[2]
CHAKRAVATHY S,GOLDBERG U,PEROOMIAN O,et al. Some algorithmic issues in viscous flows explored using a unified-grid CFD methodology: AIAA 1997-1944 [R]. 1997.
[3]
DOUGHERTY F C,KUAN Jyh-Horng. Transonic store separation using a three-dimensional chimera grid scheme: AIAA 1989-0673 [R]. 1989.
[4]
杨小亮. 飞行器多自由度耦合摇滚运动数值模拟研究 [D]. 长沙: 国防科学技术大学,2012: 46-47.
[5]
LIJEWSKI L,SUHS N. Chimera-eagle store separation: AIAA 1992-4569 [R]. 1992.
[6]
MCCOY Robert L. The aerodynamic characteristics of 7. 62 mm match bullets: ADA 205 633 [R]. 1988.
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