期刊论文详细信息
Defence Science Journal | |
Stability Criterion for a Finned Spinning Projectile | |
S. D. Naik1  | |
[1] Institute of Armament Technology, Pune | |
关键词: Gun projectiles; Aerodynamic stablisation; Free flight rockets; Sabot projectiles; Aerodynamics; | |
DOI : | |
学科分类:社会科学、人文和艺术(综合) | |
来源: Defence Scientific Information & Documentation Centre | |
【 摘 要 】
The state-of-the-art in gun projectile technology has been used for the aerodynamic stabilisation.This approach is acceptable for guided and controlled rockets but the free-flight rockets suffer from unacceptable dispersion. Sabot projectiles with both spin and fms developed during the last decadeneed careful analysis. In this study, the second method of Liapunov has been used to develop stability criterion for a projectile to be designed with small fins and is made to spin in the flight. This criterion is useful for the designer.
【 授权许可】
Unknown
【 预 览 】
Files | Size | Format | View |
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RO201912010140388ZK.pdf | 437KB | download |