Home / GATE 2017-2018 / GATE Aeronautical Engineering :: Discussion

Discussion :: GATE Aeronautical Engineering

  1. For a wing of aspect ratio AR, having an elliptical lift distribution, the induced drag coefficient is (where CL is the lift coefficient)
  2. A.
    CL/∏AR
    B.
    C2L/∏AR
    C.
    CL/2∏AR
    D.
    C2L/∏AR2

    View Answer

    Workspace

    Answer : Option B

    Explanation :

    -NA-


Be The First To Comment