Flight dynamics characteristic of tilt rotor aircraft

SHA Hong-wei; CHEN Ren-liang

Chinese

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Flight dynamics characteristic of tilt rotor aircraft

更新时间：2026-07-07

- Flight dynamics characteristic of tilt rotor aircraft
- Vol. 27, Issue 4, (2012)
- 作者机构：
  
  南京航空航天大学航空宇航学院直升机旋翼动力学国家级重点实验室,南京,210016
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2012
- 稿件说明：
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SHA Hong-wei, CHEN Ren-liang. Flight dynamics characteristic of tilt rotor aircraft[J]. 2012, 27(4).
DOI：

SHA Hong-wei, CHEN Ren-liang. Flight dynamics characteristic of tilt rotor aircraft[J]. 2012, 27(4). DOI：

摘要

总结和分析了旋翼、机翼、机身、短舱和尾翼气动力模型和操纵机构特点

其中旋翼气动力模型以准定常叶素理论为基础

机翼和尾翼气动力模型以升力线理论为基础

并分析了旋翼尾流对机翼气动力气动干扰问题;建立了全量非线性倾转旋翼机飞行力学模型;以XV-15为样机

对倾转旋翼机在不同飞行模式和飞行速度下飞行力学特性展开了详细研究

得到的结论有助于深入了解倾转旋翼机飞行力学特性

也可用于倾转旋翼机飞行控制系统设计.

Abstract

A flight dynamics model of the tilt rotor aircraft was established based on the research into the aerodynamic of the rotors

wing

fuselage

nacelle

empennage and control system.Quasi-steady element theory was used to analyze the lift

drag

moment and the flapping motion of the rotors.The lift line theory was used to research the aerodynamics of others

and then an investigation was conducted on the XV-15 tilt rotor aircraft.The results can be helpful to realize the characteristics of tilt rotor aircraft

also be useful to flight control design.

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Related Author

Xingda CUI

Lu ZHANG

Fan LIU

Shuai MA

Zhongyun XIAO

Yonggang YU

Renliang CHEN

Zhiming YU

Related Institution

Computation Aerodynamics Institute，China Aerodynamics Research and Development Center

State Key Laboratory of Aerodynamics，China Aerodynamics Research and Development Center

National Key Laboratory of Science and Technology on Rotorcraft Aeromechanics，College of Aerospace Engineering，Nanjing University of Aeronautics and Astronautics

Rotor Aerodynamics Key Laboratory,Low Speed Aerodynamics Institute,China Aerodynamics Research and Development Center

National Key Laboratory of Science and Technology on Rotorcraft Aeromechanics,College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics

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