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Flow Structure behind a Wing at High Reynolds Numbers

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  • معلومة اضافية
    • بيانات النشر:
      EDP Sciences, 2018.
    • الموضوع:
      2018
    • نبذة مختصرة :
      The stereo PIV measurement were performed behind a wing in the plane perpendicular to the flow to study the vortical structures oriented in the streamwise direction, which take place both in suction and pressure sides of the wing. The Reynolds numbers during the experiments in the 3 m wind tunnel range from 0.5 million up to 1.5 million.
    • File Description:
      application/pdf
    • Rights:
      OPEN
    • الرقم المعرف:
      edsair.doi.dedup.....6ceb68ffa8c8e9621eb955a1f27ecf3f