摘要
推导了斜筋斗计算公式 ,并计算分析了其速度、高度特性 ,及轨迹平面倾斜角、过载对斜筋斗的影响 ,计算结果与理论分析一致。
The equation about the loop maneuver of an aircraft in an inclined plane is derived.Its dynamic characteristics involved with speed and altitude,the influence of the inclined angle of the trajectory plane and load on it are also calculated and analyzed in this paper.The analysis shows that the results are correct.
出处
《空军工程大学学报（自然科学版）》
CSCD
2000年第2期8-10,共3页
Journal of Air Force Engineering University(Natural Science Edition)
关键词
斜筋斗
轨迹滚转角
轨迹平面
loop in an inclined plane；trajetory roll angle；trajectory plane
