南京航空航天大学学报（英文版）2006，Vol.23Issue(3)：161-167,7.
直升机模式下倾转旋翼机多体气弹动力稳定性分析
MULTI-BODY AEROELASTIC STABILITY ANALYSIS OF TILTROTOR AIRCRAFT IN HELICOPTER MODE
摘要
Abstract
The multi-body analysis of the aeroelastic stability of the tiltrotor aircraft is presented. Multi-body dynamic differential equations are combined with the equations of the unsteady dynamic inflow model to establish the complete unsteadily aeroelastic coupling analytical model of the tiltrotor. The stability of the tiltrotor in the helicopter mode is analyzed aiming at a semi-span soft-inplane tiltrotor model with an elastic wing. Parametric effects of the lag stiffness of blades and the flight speed are analyzed. Numerical simulations demonstrate that the multi-body analytical model can analyze the aeroelastic stability of the tiltrotor aircraft in the helicopter mode.关键词
倾转旋翼机/直升机/气弹稳定性/多体动力学/动力入流Key words
tiltrotor/helicopter/aeroelastic stability/multi-body dynamics/dynamic inflow分类
航空航天引用本文复制引用
董凌华,杨卫东,夏品奇..直升机模式下倾转旋翼机多体气弹动力稳定性分析[J].南京航空航天大学学报（英文版）,2006,23(3):161-167,7.基金项目
Supported by the "863" National High Technology Research and Development Program(863-705).国家"八六三"高技术研究发展计划资助项目. （863-705）
