2) composite aileron
复合材料副翼
1.
The simulation study of the static test of composite aileron is carried out.
对复合材料副翼静力试验进行仿真研究。
3) composite wing
复合材料机翼
1.
Rapid cost estimation for composite wings based on CAD model
基于CAD模型的复合材料机翼成本快速估算
2.
There exist several papers~() on optimizing layer design of skin of composite wing structure;but,in our opinion,they are very inconvenient as a practicable design method.
针对文中的优化方法,以复合材料机翼盒段蒙皮铺层优化为例进行了数值计算,通过优化计算验证了该方法有较高的效率,对工程设计具有一定的应用价值。
3.
A design study aimed to optimize a composite wing in an aeroelastic way was presented using genetic algorithm and genetic/sensitivity-based hybrid algorithm.
利用遗传算法和遗传/敏度混合优化算法对某复合材料机翼进行气动弹性优化设计研究,并提出在使用这两种算法时根据设计敏度信息计算设计变量的重要性指标、从而确定主要和次要设计变量、进而调整设计变量变化域的方法,以提高算法的寻优效率。
4) all composites wings
全复合材料机翼
1.
Finite element analysis for all composites wings of UAV
无人机全复合材料机翼的结构有限元分析
5) forward swept wing
前掠翼
1.
The divergence experiment prediction techniques of flat plate forward swept wings are presented.
介绍了平板前掠翼的发散试验技术。
6) forward-swept wing
前掠翼
1.
The W-shaped tailless aircraft has not stabilizer and vertical tail,and it is based on the design of forward-swept wing and the integrated design of blended wing-fuselage.
W型无尾飞机基于前掠翼及翼身融合的一体化设计,取消了平尾和垂尾,可大幅降低雷达反射截面积,减轻结构重量;同时具有亚声速气动效率高、横航向操纵面效率高的优势。
2.
The authors investigate experimentally the effect of canard wing and sweep angle on longitudinal aerodynamic characteristics of canard-forward-swept wing configuration by means of forces measurement in wind tunnel.
前掠翼布局由于其潜在的优势,在未来战斗机的研制中将占有日益重要的地位。
3.
Its design idea is based on the flow behavior of forward-swept wing and the flow control concept.
提出了一种新型的飞机气动外形—— W-型无尾布局及其气动设计思想 ,初步研究了两种气动布局方案 :前掠翼无尾气动布局和 W-型无尾气动布局。
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。
参考词条