Scholarlink

In this paper, an electric vector composite thrust aircraft is designed, which takes into account the functions of vertical take-off and landing and high-speed forward flight. A configuration scheme of coaxial dual rotor, fixed wing and tail thrust propeller is proposed, and the coaxial dual rotor airfoil is determined by aerodynamic design. The numerical simulation calculation is carried out for the fuselage, the horizontal and vertical tails, and the aerodynamic parameter characteristics are analyzed. The aerodynamic characteristics of coaxial dual rotor blades are clarified. The conclusion that the overall design scheme basically meets the requirements of the overall parameters is obtained, which provides a reference for the subsequent optimization iterative design and the research of UAV control method.

错误：搜索内容不能为空，请输入英文关键词
错误：关键词超出字数限制，请精简
高级检索

Overall Design and Aerodynamic Characteristics Analysis of an Electric Composite Thrust Aircraft

  • 会议论文

  • 发表日期：

    2026年

查看全文
  • Chang Fu,
  • Minglong Pan,
  • Weitian Zhang,
  • Peng Qin,
  • Dongdong Zhu

摘要

In this paper, an electric vector composite thrust aircraft is designed, which takes into account the functions of vertical take-off and landing and high-speed forward flight. A configuration scheme of coaxial dual rotor, fixed wing and tail thrust propeller is proposed, and the coaxial dual rotor airfoil is determined by aerodynamic design. The numerical simulation calculation is carried out for the fuselage, the horizontal and vertical tails, and the aerodynamic parameter characteristics are analyzed. The aerodynamic characteristics of coaxial dual rotor blades are clarified. The conclusion that the overall design scheme basically meets the requirements of the overall parameters is obtained, which provides a reference for the subsequent optimization iterative design and the research of UAV control method.