摘要
该文根据烧蚀模型计算出弹丸在某一时刻的烧蚀外形及其对应的气动系数 ,利用外弹道模型仿真高超声速弹丸烧蚀后对其外弹道特性的影响。文中所采用的理论。
On the basis of ablation model, the paper calculated the ablation shape of projectile at a certain time, and computed corresponding aerodynamic coefficients.Using outer ballistic trajectory model,the paper simulated the effect on the outer ballistic trajectory characteristics after the ablation of hypersonic projectile. The theory, method and calculation results presented in the paper are valuable for the study of hypersonic projectiles in the future.
出处
《南京理工大学学报》
EI
CAS
CSCD
北大核心
2002年第3期247-250,共4页
Journal of Nanjing University of Science and Technology
基金
国防科技预研行业基金资助项目
关键词
高超声速弹箭
弹丸
烧蚀
外弹道特性
气动系数
projectiles, ablation,exterior ballistic characteristics
hypersonic