摘要
基于大攻角飞行条件下的动力学方程,定性分析了飞机在大攻角条件下作俯仰飞行的动力学特性。提出了在不同参数匹配条件下的飞行稳定性,并据此划分了飞机的飞行稳定域。
Based on dynamics equation of aircraft flying at high angles of attack, the dynamical characteristics of aircraft flying at pitching on condition of high angles of attack are qualitatively analyzed. The flying stabilities are raised on the basis of various matching parameters, and then the stable field of aircraft can be divided.
出处
《空军工程大学学报（自然科学版）》
CSCD
北大核心
2006年第4期11-12,16,共3页
Journal of Air Force Engineering University(Natural Science Edition)
关键词
大攻角
俯仰飞行
稳定域
high angle of attack
pitching flying
stable field
