摘要
为了解复合升力体飞行器的飞行特性,以及不同升力面之间的气动干扰特性,在小型模型飞机的基础上研制了复合升力体飞行器验证机,并开展了一系列的试飞研究。试飞结果表明,飞行器旋翼模式和固定翼模式之间的过渡飞行完全可控,过程平稳,旋翼与固定翼升力面之间无不利干扰。
In order to understand flight characteristics and aerodynamic interactions between different lift surfaces of compound lifting-body aircraft,a flight demonstrator has been developed on the basis of subscale model aircraft and a series of flight tests has been conducted.The flight test results show that,the transition flight between rotary-wing flight mode and fixed-wing flight mode is completely controllable and the transition process is smooth,there is no adverse interference between lift surfaces of rotary wing and fixed wing.
出处
《飞行力学》
CSCD
北大核心
2013年第2期167-169,共3页
Flight Dynamics
关键词
复合升力体飞行器
飞行特性
气动干扰
验证机
试飞研究
compound lifting-body aircraft
flight characteristics
aerodynamic interference
flight demonstrator
flight test research
