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结合旋翼和固定翼的飞行特点,提出了一种可以在垂直起降和水平飞行之间切换状态的飞行器布局。围绕该类飞行器的力学特性、气动特性作出了分析和计算,并根据分析和计算的结果,制作并试飞了实物模型。根据研究结果做出的实物样机试飞参数与理论结果符合较好,初步达到了设计目的,证实了这种飞行器布局具有一定的可行性和应用前景。
Combining the flight characteristics of rotor and fixed wing, an aircraft layout that can switch state between vertical takeoff and landing and horizontal flight is proposed. Based on the mechanical characteristics and aerodynamic characteristics of the aircraft, the aerodynamic characteristics were analyzed and calculated. Based on the analysis and calculation results, the physical model was produced and tested. According to the results of the research, the flight test parameters of the physical prototype are in good agreement with the theoretical results, which have initially achieved the design purpose and confirmed the feasibility and application prospect of this aircraft layout.