1) joined-wing
连翼
1.
To our knowledge,there are very few papers on the aeroelastic tailoring of composite joined-wing aircraft,although it is key to the design of such aircraft.
应用MSC/NA STRAN软件的气弹优化模块,对一个真实的复合材料连翼结构,采用分步实现的策略进行了连翼在颤振/发散速度约束下的气动弹性剪裁。
2) joined wing
连翼布局
1.
On the basis of collecting,trimming,and analyzing the overseas research information about joined wing aircraft,this paper presents the research history and design characteristics of joined wing aircraft.
在收集、整理、分析国外连翼布局飞机研究资料的基础上,介绍了国外连翼布局飞机的研究历程和设计特点;特别是基于近年来对未来战场信息情报、监视、侦察任务的需求,介绍了连翼布局探测无人机这一新的作战概念和装备技术的研究进展情况。
2.
In the design of joined wing, the complex and the interaction between each specialities and subjects are unknown from previous design experience.
连翼布局飞机设计中,各专业学科之间的相互影响和复杂性是以前的设计中所未知的。
3) wing pole
连翼杆
1.
In developing course the rocket engine of certain flight-assisted equipment’s empennage wing pole whorl root part splits leads to the shell body fly not steadily occurs many times.
分析了某型助飞发动机的喷管与尾翼连翼杆组件的温度与应力场,找到了多次发生火箭发动机尾翼连翼杆螺纹根部处断裂的问题所在,给出了解决方案。
补充资料：变后掠翼飞机(见后掠翼飞机)
变后掠翼飞机(见后掠翼飞机)
swing-wing aircraft
bianhoul位eyi feiii变后掠翼飞机(swing一wing aircran)见后掠翼飞机。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。