Induced drag occurs at low speeds and at higher speeds as, at wing tips, air moves from the area of high pressure to the area of low pressure.

誘導(dǎo)阻力發(fā)生在低速和在更高的速度被操高潮了视频，在機(jī)翼的秘訣，空中動(dòng)作插入美女国产，從該地區(qū)的高壓力日韩欧美久久精品影视大全免费观看，向低壓區(qū)的壓力。

This configuration can theoretically provides 50% reduction of induced drag through varying the lift distribution between the two wings.

在理論上通過改變2個(gè)機(jī)翼之間的升力分布可以使得飛機(jī)的誘導(dǎo)阻力有較大減少免费AV免费网站。

The accurate prediction of drag is key to the design of the low Reynold′s number flight vehicle,and the accurate prediction of friction drag which is induced by separation and transition of the boundary layer is key to the accurate prediction of drag.

而與附面層分離和轉(zhuǎn)捩相關(guān)的摩擦阻力的精確計(jì)算則是此類飛行器阻力精確計(jì)算的關(guān)鍵主播一多大秀喷水视频。

At an altitude of 1/10 wingspan, however, induced drag is decreased by half.

在翼展十分之一高度的時(shí)候中国欧美亚洲范冰冰与中字，誘導(dǎo)阻力減少了一半。

In theory, oblique elliptic wing with an elliptic load has the minimum wave drag due to lift and induced drag.

理論分析表明欧美亚洲日韩，具有橢圓載荷分布的斜置橢圓機(jī)翼有最小的升致波阻和誘導(dǎo)阻力99在线视屏。

induced drag：誘導(dǎo)阻力

飛機(jī)飛行時(shí)所產(chǎn)生的阻力主要是來自蒙皮磨擦阻力(skin friction drag)及誘導(dǎo)阻力(induced drag). 阻力對一般次音速飛機(jī)的航程與飛行性能影響甚大. 由阻力概觀(見參考資料4.)研究論文中,可以概略了解飛機(jī)巡航時(shí)各種阻力分布的情形(見圖一).

induced drag：誘導(dǎo)抗力

制圖;繪圖 drawing | 誘導(dǎo)抗力 induced drag | 輔助投影 auxiliary projection

induced drag：誘導(dǎo)曳力

抽氣通風(fēng) induced draft | 誘導(dǎo)曳力 induced drag | 誘導(dǎo)速度 induced velocity

induced drag：誘導(dǎo)阻力;引發(fā)阻力

induced dipole 感應(yīng)偶極 | induced drag 誘導(dǎo)阻力;引發(fā)阻力 | induced drag coefficient 誘導(dǎo)阻力系數(shù);引發(fā)阻力系數(shù)

induced drag coefficient：誘導(dǎo)阻力系數(shù)

induced drag ==> 誘導(dǎo)阻力 | induced drag coefficient ==> 誘導(dǎo)阻力系數(shù) | induced draught ==> 誘導(dǎo)通風(fēng)