只用翼梢碰他一下！
翼梢小翼影响一部分名为诱导阻力的阻力。
因此，采用伸缩栅格的变体翼梢小翼具有改善飞机起飞性能的潜力。
Therefore, morphing winglet with retractable grid has the potential of improving aircraft takeoff performance.
跟着，他毫不犹豫地紧收前翼，展开短短的。 弯成角度的翼梢，径直向海面扑去。
Then without ceremony he hugged in his forewings, extended his short, angled wingtips, and plunged direcfly toward the sea.
我缺的就是一对短小的翅膀，我该做的就是尽可能收拢双翅，只用翼梢飞行！
All I need is a tiny little wing, all I need is to fold most of my wings and fly on just the tips alone!
他没有几个席卷低水平库通行证以及他例行商标特技完成烟雾滤毒罐的翼梢。
He did several sweeping low-level banked passes as well as his trademark aerobatic routine complete with smoke from the wingtip canisters.
成功的实例设计结果表明，本文方法对民用飞机机翼-翼梢小翼的设计具有应用价值。
The results of practical design showed that this method can be used in the design of winglet.
以某型双发低速飞机为例，对剪切翼梢装置对飞机滚转性能的影响进行了理论研究和分析。
In the paper, as an example by some type low speed twin-engine airplane, theoretical research and analyses about the effect of the tip unit of a sheared wing on airplaneroll performance are conducted.
如此卓著的效率应当归功于低阻机翼、前缘缝翼和双开缝襟翼，以及高马赫混合式翼梢小翼。
This efficiency is due largely to the innovative design of the low-drag wing. This design includes leading-edge slats, double-slotted Fowler flaps, and high-Mach blended winglets.
该文应用低阶速度势面元法建立了预报三维水翼水动力性能的数值方法，重点对翼梢和尾涡进行了研究。
A potential-based surface panel method is applied to predicting the performance for three-dimensional hydrofoils, with emphasis on the tip region.
为了提高数值计算效率和准确性，提出了基于多级响应面法的确定翼梢小翼气动外形参数的一种优化方法。
In order to improve the efficiency and accuracy of the numerical calculation for the aerodynamic design of winglets, an optimization method based on multi-level response surfaces is proposed.
利用在一个机翼翼梢安装的翼梢小翼形成受扰动旋涡，在风洞和水洞中对受扰动涡的自组织过程进行了测量。
The self-organization of vortices disturbed by different taps are measured both in wind tunnel by PIV and in water tunnel by LDV.
“你们整个身体，从这边翼梢到那边翼梢，”又有一次乔纳森又这么说，“就是你们的思想本身，只不过变成了你们肉眼看得见的形式罢了。”
"Your whole body, from wingtip to wingtip," Jonathan would say, other times, "is nothing more than your thought itself, in a form you can see."
对翼身组合体等弦长大展弦比超临界机翼，除翼梢处流动三维效应强外，机翼其余部分包括接近翼根附近，均具有近似二维流动的特征。
Most part of the supercritical wing with equal chord and high aspect ratio is provided with 2-D flow characteristics approximately except wing tip.
对翼身组合体等弦长大展弦比超临界机翼，除翼梢处流动三维效应强外，机翼其余部分包括接近翼根附近，均具有近似二维流动的特征。
Most part of the supercritical wing with equal chord and high aspect ratio is provided with 2-D flow characteristics approximately except wing tip.
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