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超轻型飞机是通用航空技术发展的方向之一。统计国外超轻型飞机的性能参数,得到翼载荷和重功比与飞机的最大平飞速度、失速速度、起飞距离、爬升率的关系。针对这些关系式,结合超轻型飞机的设计要求,提出一套超轻型飞机设计参数选取的方法。此方法不只是限于超轻型飞机,对其他类型的飞机同样适用。
Ultralight aircraft is one of the directions for the development of general aviation technology. Statistics of the performance parameters of foreign ultralight aircraft, the wing load and rework ratio and the maximum plane flying speed, stall speed, takeoff distance, climb rate relationship. In view of these relations, combined with the design requirements of the ultralight aircraft, a method for selecting the design parameters of the ultralight aircraft is proposed. This method is not limited to ultralight aircraft and is equally applicable to other types of aircraft.