An analysis of constructions and attachment forms of wing-to-fuselage attachment fitting for modern fighters is carries out in this paper.
较详细分析了现代战斗机翼-身接头的构造和连接形式以及各种形式的优缺点和选择这些结构形式时的注意事项,并对现代战斗机翼-身接头形式未来的发展趋势作出预测。
In this paper, technical data have been obtained precisely by computing and analyzing the structure of wing joint with finite element method.
通过对机翼接头结构的有限元分析计算 ,得到接头各部分的应力数值 。
2g/L f or 5min in the treatment of primary and recurrent double-head pterygia.
2g/L丝裂霉素C(MMC)5min治疗原发性和复发性双头翼状胬肉的效果和复发率。
The improved cylindrical wing-form bit has 18 diamond tungsten carbide composite button bits and 3 button bits more than the original drilling bit,with drilling cutters arranged according to the force on bit.
改进型筒形翼状钻头比原先使用的平底滚刀钻头增加了18个孕镶金刚石-针状硬质合金复合式钻齿和3个钎头,并按受力特点进行了合理分布。
Strength analysis and optimization design for wing joint based on ANSYS
基于ANSYS的机翼接头强度分析及优化设计
wing attachment
机翼连接接头机翼的固定
Nonlinear Finite Element Analysis of Wing-Fuselage Connection Joint
机翼机身对接接头非线性有限元分析
wing-to-fuselage fairing
机翼机身接合整流带
(especially of aircraft wings) angled rearward from the point of attachment.
（尤指飞机机翼）从连接点向后转变角度。
Cement the fuselage bottom cover and wing together as shown in the diagram.
再将机身下罩按图示粘接在机翼上。
Aerofoil Sub-wainscot Wing-rib Join-hole Structure Fracture Characteristics Research Based on 3D Contact Problem
含三维接触问题的机翼下壁板翼肋对接孔结构断裂特性研究
a straight line connecting the leading and trailing edges of an airfoil.
连接机翼的前缘与后缘的直线.
A Study on Integrated Aerodynamic/Structural Design of Joined-Wing Aircraft;
联接翼飞机气动/结构一体化设计研究
With much caution he climbed to the top of the wall.
他小翼翼地爬上墙头。
A better location would have been near the nose, ahead of the wing.
更佳的位置应该在机头附近，机翼的前面。
fuselage-wing-tail combination configuration
机身－机翼－尾翼组合体
(A thousand years later, in 1804, Napoleon I was careful to take the crown from the Pope's hands and place it on his own head. )
(一千年后的1804年，拿破仑一世小心翼翼地从教皇手上接过皇冠，把它戴在自己的头上。)
Remove 'H' coupling bolts from A/C compressor side of coupling.
从A/C压缩机接头侧拆下 'h'接头螺栓。
Assembly consists of thumb screw, hooks, swivel joint, and stem, threaded at one end.
这种总成由翼型螺丝、钩、转接头和杆子组成，在一端上有螺纹。
The receiver aircraft is fitted with a probe that extends out from the side of the fuselage or from the leading edge of the wing.
受油机装备有一个从机身一侧或者是机翼前缘伸出的探头。
camber changing flap
改变机翼弯度的襟翼
main foil flap hydraulic actuator
主翼襟翼液压执行机构