A Estimation Method for Projectile Stability Based on Numerical Virtual Flight Technology
Received date: 2016-04-21
Online published: 2025-05-23
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
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.
| [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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