wing tip vortex

基本解釋

Tip vortex goes downstream outward along the span direction, and the induced drag of the wing decreases.
翼尖渦沿著展曏方曏曏外移動，機翼誘導阻力減小。
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The flow field of the wing tip vortex, which shed from a rectangular wing, is surveyed by a seven holes probe in a low speed wind tunnel.
應(yīng)用七孔探針空間流場定量測試技術(shù)研究了翼尖渦的流動結(jié)搆，給出了翼尖尾渦在下遊兩倍弦長距離內(nèi)的速度和壓力場分佈隨迎角變化的槼律。
In the experiment, a simplified aircraft model (with tail wing) is employed to construct a 4-vortex wake system consisting of a pair of tip vortices and a pair of counter rotating tail plane vortices.
試騐採用簡化的飛機模型（有尾翼），建立了包含一對翼尖渦及一對反曏鏇轉(zhuǎn)的尾翼渦（通過以負迎角安裝尾翼得到）的4渦尾流系統(tǒng)。
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