Matching the Lift in order to calculate the flap angle

    • Marco Peviani

      Hi everyone, I have a NACA 4410 profile which I have done an analysis at different AoA (parameterizing the AoA) to find the CL and the CD. Now I want another run but with a 2410 with flaps, matching the lift from the first analysis to get the flap angle to have the same LIft.

      For example I have the 4410 at 5° of AoA and I find that the CL is 0.93, now with the same CL I want to find the Flap angle (of 2410).

      How can I do ?
      Thanks in advance

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