Compute Wing Maximum Lift Coefficient (CL)

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  • Опубликовано: 8 ноя 2019
  • Find out how to compute the maximum lift coefficient on a 3D wing using 3DFoil software.
    More information can be found at: www.hanleyinnovations.com/3dfo...
  • НаукаНаука

Комментарии • 2

  • @professionalprocrastinator8103
    @professionalprocrastinator8103 Год назад +1

    Which model are you using for the stall correction Dr. Hanley?
    Nice video btw

    • @hanleyinnovations
      @hanleyinnovations  Год назад

      Thanks. I am using a stall model based on the airfoil (at midspan) boundary layer separation.