wing tip vortex

基本解释

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.
應用七孔探針空間流場定量測試技術研究了翼尖渦的流動結搆，給出了翼尖尾渦在下遊兩倍弦長距離內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的尾翼渦（通過以負迎角安裝尾翼得到）的4渦尾流系統。
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