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1)  wing-tip aileron; rotating wing-tip
翼尖副翼
2)  all-moving tip of wing
翼尖的副翼<火>
3)  interplane aileron (of biplane)
翼间副翼
4)  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。
5)  aileron [英]['eɪlərɔn]  [美]['elə'rɑn]
副翼
1.
The computation of a wing-body combination with aileron;
带副翼的翼身组合体的数值模拟
2.
The feasibility analysis of aileron manpower control in a fighter;
某型歼击机副翼人力操纵可行性分析
3.
The flows around 2-D and 3-D wings with ailerons deflected are numerical simulated in cases of subsonic, transonic and supersonic speeds.
数值模拟了带副翼偏转构型的二维、三维亚、跨、超声速来流情况的绕流流场,采用有限体积方法和AUSM+迎风格式数值求解N-S方程,四步龙格-库塔时间推进,湍流模型为Baldwin-Lomax和Spalart-All-maras湍流模型。
6)  tapered wing
尖翼
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。
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