稳定尾旋特性研究的一种计算图解法  

A CALCULATIVE—GRAPHICAL METHOD IN RESEARCH FOR CHARACTE—RISTICS OF STEADY SPIN

作　　者：徐邦年[1] 

机构地区：[1]空军指挥学院,北京100081

出　　处：《飞行力学》1993年第4期21-30,共10页Flight Dynamics

摘　　要：按稳定尾旋的条件对飞机运动方程组作了简化。提出一种计算图解法和尾旋中侧滑角计算式,并用于J—7飞机稳定尾旋特性研究和验证。In this paper, the non—linear differential equations of aircraft motion are simplified by the condition of steady spin. Put forward a calculative—graphical method and calculative equation of sideslip angle. The method and equ(?)ation of sideslip angle are used to the research of characteristics of stead spin of aircraft J—7. The method and equation of sideslip angle are testified to avaiable.

关 键 词：稳定尾旋 侧滑角 计算图解法 飞机 

分 类 号：V212.11[航空宇航科学与技术—航空宇航推进理论与工程]