摘要
根据舰载飞机的动力学方程,计算了示例飞机起飞离舰后的过舰首下沉量。对离舰速度、离舰迎角、飞机总重力、甲板风和预置舵偏度等影响因素作了计算和分析,最后确定了飞机的最小弹射末端速度。
In this paper, the—over—the—bow of a example airplane are calculated by longitudinal dynamical equations for a carrier based airplane, The influence factors, such as take—off speed, take— off angle of attack, gross weight of airplane, wind over the deck, presetting elevator deflection, are calculated and analyzed. The minimum catapulting endspeed for the airplane is determined.
出处
《飞行力学》
CSCD
北大核心
1993年第3期42-49,共8页
Flight Dynamics
关键词
舰载飞机
过舰首下沉量
速度
Carrier based airplane Sink—over—the—bow Minimum catapulting endspeed
