摘要
本文根据空气动力学理论和超音速弹丸的激波特性,建立了在使用L型立靶基础上正向射击和任意角度射击时的数学模型,并进行了误差分析,提出了减小误差的修正方法。
Based on aerodynamic theory and the characteristics of the shockwave around a supersonic projectile, the article constructs a mathematical modeling of a L-shaped vertical target for projectiles shooting with forward direction and any direction, and analyzes the error sources and provides correcting ways to lower the error.
出处
《应用声学》
CSCD
北大核心
2006年第4期252-257,共6页
Journal of Applied Acoustics
关键词
声学立靶
脱靶量测试
模型
误差分析
Acoustic vertical target, Target deviation measurement, Model, Error analysis
