摘要
根据地面效应的特点及相似准则,给出了基于展弦比、梢根比和机翼离水相对高度等参数的盒式翼外形简化设计原则。针对地效飞行器高度焦点配置,结合盒式翼外形简化设计原则,给出了盒式翼纵向位置的简化设计方案。针对盒式翼地效飞行器在起飞过程中的升阻特性,给出了发动机类型选择及动力配置的优选方案。针对地效飞行器的飞行特点,阐述了盒式翼地效飞行器机身和尾翼的设计要点。通过以上分析为基于盒式翼的地效飞行器气动布局概念设计提供了设计依据和参考。
Firstly,the simplified principles of box wing configuration design are presented based on aspect ratio,taper ratio and relative flying height of wing above the water surface,as well as characteristics and similarity criterions of ground effect. Secondly,the simplified design method of longitudinal stations of box wing is proposed considering the focus of flying height of wing-in-ground effect vehicle( WIG) and principles above. Thirdly,the optimization scheme on engine propulsion type and power deploying is given according to the lift-drag characteristics during the taking-off mission of WIG. Finally,fuselage and tail design of WIG are briefly described,taking its flight characteristics into consideration. Therefore,the analysis above can be taken as the basis during the aerodynamic configuration conceptual design of WIG based on box wing.
出处
《南京航空航天大学学报》
EI
CAS
CSCD
北大核心
2017年第S1期6-11,共6页
Journal of Nanjing University of Aeronautics & Astronautics
关键词
气动布局
概念设计
盒式翼
地效飞行器
地面效应
aerodynamic configuration
conceptual design
box wing
wing-in-ground effect vehicles(WIG)
ground effect
