首页 | 本学科首页   官方微博 | 高级检索  
     检索      

联结翼飞机布局特点探讨
引用本文:郭卫刚,余雄庆.联结翼飞机布局特点探讨[J].海军航空工程学院学报,2005,20(2):201-204.
作者姓名:郭卫刚  余雄庆
作者单位:海军航空工程学院飞行器工程系 烟台(郭卫刚),南京航空航天大学航空宇航学院 264001(余雄庆)
基金项目:航空科学基金资助项目(00B52017)
摘    要:联结翼飞机是一种新型的飞机布局形式,具有与常规飞机不同的特点。文章从结构、气动、操纵控制的角度对联结翼布局飞机进行了分析。通过分析表明,联结翼飞机与常规飞机相比具有重量轻、强度刚度大、阻力低、较大的升力和直接力控制的优点。对联结翼飞机布局特点进行探讨可为今后新概念飞机设计提供参考。

关 键 词:联结翼布局  气动特性  直接力控制
修稿时间:2004年11月30

A Discussion on the Characteristics Of the Joined-Wing Airplane Configurations
GUO Wei-gang,YU Xiong-qing.A Discussion on the Characteristics Of the Joined-Wing Airplane Configurations[J].Journal of Naval Aeronautical Engineering Institute,2005,20(2):201-204.
Authors:GUO Wei-gang  YU Xiong-qing
Institution:GUO Wei-gang,YU Xiong-qing Department of Airborne Vehicle Engineering,NAEI,Yantai,264001 College of Aerospace Engineering,NUAA,Nanjing,210016
Abstract:The joined-wing airplane is a sort of new configuration airplane; it is different from conventional airplane. This paper discusses the characteristics of the joined-wing configurations from viewpoints of structure, aerodynamics and control. It indicates that the joined-wing airplanes have many advantages, such as lighter structure, more strength and rigid structure, lower drag and larger lift than conventional configuration, as well as the ability of direct force control. Discussion on the joined-wing can offer reference to new concept airplane.
Keywords:joined-wing configuration  aerodynamics characteristics  direct force control
本文献已被 CNKI 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号