摘要
通过对某飞翼飞机输油顺序的研究,分析了在不同输油顺序下飞机重心的变化情况及在不同重心位置下升降舵偏转角和飞翼飞机的配平状况。通过对最小配平阻力和飞机最佳重心位置的研究可知,改进飞机的输油顺序,可以增加飞机的巡航时间并改善飞机的操纵能力。
Based on a flying-wing aircraft of oil order to analyze the gravity center＇ s change of the aircraft in different oil order, and the elevator angle and flying-wing aircraft trim conditions in different centre-of-gravity position. Through the study of minimum trim drag and the best center of gravity of the aircraft, improve the aircraft＇ s oil order, which can increase the aircraft＇s cruising time and improve the aircraft＇s maneuvering capability.
出处
《飞行力学》
CSCD
北大核心
2011年第3期16-19,共4页
Flight Dynamics
关键词
飞翼
飞机配平
输油顺序
flying wing
aircraft trim
oil order
