1. Winglets affect the part of drag called induced drag.
翼梢小翼影响一部分名为诱导阻力的阻力。
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2. For example, it outfitted its whole fleet with rounded winglets.
例如为全部的机群配置圆形的机翼。
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3. The winglets will be used to trim aerodynamic loads if required.
如果需要，翼展将用来消弱气动荷载。
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4. This difficult problem can be solved by mounting winglets on the stabilizing wing.
采用在稳定翼上加装小襟翼的方法，即可以解决这一难题。
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5. The control method has been agreed for the "winglets" on the nose and tail of Bloodhound.
这种控制方法和猎犬号鼻翼和尾部所采用的翼翅向一致。
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6. The second variant is called "Wind Blade", and adds the extended wingspan and winglets you see above.
第二个叫做“风刃”，在其上面可以看到附加的翼展和翼翅。
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7. Flutter control of the suspension Bridges by pneumatic winglets is studied from the standpoint of energy mechanism.
从能量的角度研究气动翼板控制悬索桥颤振的物理机理。
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8. An analysis of flight test results was conducted to explain the effects of winglets on aerodynamic load, control-stability and performances.
本文对翼尖小翼的飞行试验结果进行了分析，试图说明它对飞机的气动载荷、操稳特性及飞行性能的影响。
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9. The designers quickly clawed back much of the loss, with a variety of intricate and novel solutions such as the 'horn' winglets first seen on the McLaren MP4-20.
10. A single flap replaces the previous double design and the additional winglets over the main profile have increased in length, almost reaching the side of the nosecone.
单襟翼取代了原本双襟翼的设计，同时主体上方额外的翼端帆长度也增加，现在几乎要碰到鼻锥。
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11. 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.
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。
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12. At the nurburgring , the winglets and the cooling chimneys on the ferrari \ ' s sidepods have been combined into one single element , emphasising further their aerodynamic function.
在纽柏林，法拉利侧进风口上的翼端帆和冷却用的烟囱被结合成单一物件，进一步强调其空力的作用。
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13. 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.
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。
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14. 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.
