1) small wing
小型翼
2) flat V tip vane
平板V型小翼
1.
Optimization of flat V tip vane geometry parameters were tested to upgrade power coefficient of wind turbine C_p.
为提高风力机的功率系数Cp,对平板V型小翼的参数进行了优化试验。
3) subminiature rotorcraft
超小型旋翼机
1.
A hybrid modeling method of a subminiature rotorcraft in horizontal turning had been proposed by using mechanism model and NN-compensation.
采用神经网络补偿机理模型法进行超小型旋翼机系统的平面转弯运动建模。
2.
The dynamics of a subminiature rotorcraft was given including flybar’s flapping.
针对复杂的超小型旋翼机系统,利用牛顿-欧拉方法建立了其系统动力学模型,包括了希勒翼的动力学;为了简化控制器设计,利用奇异扰动理论,把复杂的动力学模型降阶为两个子系统,即平移动力学和姿态动力学;采用非线性逆动力学设计了输出跟踪控制器。
3.
A model for the nonlinear dynamics of a subminiature rotorcraft is established.
建立了超小型旋翼机系统的非线性参数化模型。
4) On Transformation of Left-Wing Fiction
左翼小说的转型
5) winglet
[英]['wiŋlit] [美]['wɪŋlɪt]
翼梢小翼
1.
The optimal design of civil aircraft winglet with multiple constraint;
民用飞机翼梢小翼多约束优化设计
6) winglet
[英]['wiŋlit] [美]['wɪŋlɪt]
翼尖小翼
1.
To match these needs,a bigger wing aspect ratio and winglet are adopted as the improvement measures,hopefully the lift-drag ratio of the modified UAV could be increased.
为延长某无人机的留空时间,加大航程和提高升限,用适当加大机翼展弦比和加装翼尖小翼的办法对原型机的气动特性进行了改进,以期能使该无人机的升阻比有较大提高。
2.
Modification of winglet is adopted to raise the lift-drag ratio of the UAV for extension endurance,for enlarge range and for increase ceiling.
为延长无人机留空时间,加大航程和提高升限,可采用加装翼尖小翼的方法使无人机的升阻比有所提高。
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