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本文用BACTM法配合时域动态响应研究了JJ-6飞机进入和改出尾旋的操纵规律.文中所用的操纵面是方向舵和升降舵。通过计算、分析,确定出可能出现尾旋的操纵区。最后探讨了尾旋进入和改出的机理。
In this paper, the law of maneuvering into and out of the tail rotation of the JJ-6 aircraft is studied by using the time-domain dynamic response method with the BACTM method. The control surfaces used in this paper are the rudder and the elevator. Through calculation, analysis, determine the possible spin control zone. Finally, the mechanism of the entrance and exit of the tail spin is discussed.