航空工程进展2025，Vol.16Issue(4)：1-12,12.DOI:10.16615/j.cnki.1674-8190.2025.04.01
倾转旋翼机气动设计研究进展
Development in aerodynamic design of tiltrotor aircraft
摘要
Abstract
The tiltrotor aircraft has both traditional helicopter vertical takeoff and landing,airborne hovering capabi-lities,and high-speed cruising performance of fixed wing aircraft.The excellent flight performance of tiltrotor air-craft has enormous potential for development and application in the aviation field.However,at the same time,it al-so brings many challenges to research and design.The development of the overall aerodynamic configuration of til-trotor aircraft has undergone decades of iterative optimization,and there are still many key technologies in the aero-dynamic design of tiltrotor aircraft that need to be further explored.This article focuses on the research status of op-timizing the shape design of tiltrotor blades,aerodynamic interference of tiltrotor aircraft,and aerodynamic elastic stability of whirl flutter.Based on the current situation,the next step of aerodynamic design research prospect for til-trotor aircraft is discussed,and several suggestions for research directions are provided.关键词
倾转旋翼机/倾转旋翼/飞行模态/回转颤振/气动干扰Key words
tiltrotor aircraft/tiltrotor/flight mode/whirl flutter/aerodynamic interference分类
航空航天引用本文复制引用
王宗辉,杨云军,赵佳祥..倾转旋翼机气动设计研究进展[J].航空工程进展,2025,16(4):1-12,12.基金项目
国家自然科学基金(U21B2054) （U21B2054）
