摘要
本文通过舰载飞机弹射起飞动力学的研究,并根据弹射起飞的过程和要求,提出了确定弹射起飞参数(弹射力、发动机推力和平尾偏角)的计算方法。文中对舰载机的弹射起飞进行了仿真计算。最后讨论了飞机的起飞质量,发动机推力、起飞迎角、襟翼偏角和甲板风航迹等对弹射起飞性能的影响.
This paper, by investigating the catapulting dynamics of the carrier-based airplane and according to the requirements of catapult takeoff, provided a method to determine catapulting parameters(the catapult force, the thrust and the elevator angle). In this paper, the take-off path of sea-based aircraft was calculated. Finally, a brief discussion is present about the influence of the airplane gross weight, the thrust, the maximum angle of attack, the flap angle and the wind over the deck on the catapulting performence.
出处
《飞行力学》
CSCD
北大核心
1992年第3期27-33,共7页
Flight Dynamics
关键词
舰载飞机
弹射起飞
弹射性能
Carrier-based airplane Ejection take-off Take-off path Catapulting dynamics Catapulting performence
