A flow visualization investigation on leading edge breakdown is conducted in a wind tunnel to identify the effect of blowing on a strake wing model undergoing large amplitude pitching motions.

 
  • 實(shí)驗采用翼面吹氣控制翼面非定常流動(dòng),通過(guò)煙流顯示渦軌跡和渦破碎位置,用相鎖照相技術(shù)記錄空間流態(tài)。
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