本文利用经典的定常滚转稳定性理论,对滚转稳定条件作了简单的推导,在此基础上应用大型电子计算机和自编的图形打印程序对一架典型的现代歼击机的滚转特性作了详细的计算分析。研完了不同飞机设计状态下整个飞行包线范围内的快滚稳定性;发动机陀螺力矩、重心、过载变化对滚转稳定性的影响;气动阻尼、纵向和航向静稳定性匹配对滚转稳定性的作用。 In this paper, the classical steady roll stability theory is used to make a simple deduction of roll stability conditions. Based on this, the roll characteristics of a typical modern fighter plane are made using a large electronic computer and a self-designed graphics printing program Detailed calculation and analysis. After the completion of different aircraft design state of the entire flight envelope within the scope of the fast rolling stability; engine torque, center of gravity, overload changes on roll stability; aerodynamic damping, longitudinal and aerostatic stability of the stability of the roll stability Role.