对弹丸飞行稳定性进行了分析,文中提出利用M GAERO 气动软件计算弹丸的气动力参数,以减少采

用经验公式估算气动力系数和压心位置等参数带来的误差,可为弹丸飞行稳定性分析和总体参数设计提供

参考依据。-For projectile flight stability analysis, this paper proposes the use of software to calculate projectile M GAERO aerodynamic aerodynamic parameters to reduce the use of empirical estimates of aerodynamic coefficients and parameters such as pressure center position error caused by, for projectile flight stability analysis and overall parameters of the design of reference.