7 Replies Latest reply on May 9, 2008 12:28 AM by Anthony Botting

    how to generate an XY plot for lift vs airfoil chordlength?

    Tan  TS
      Hi, i'm currently using floworks to simulate a NACA0015 aorfoil. i managed to run the solver with results calculated. however, i am unable to generate an XY plot for the lift force vs the chordlength, any pointers?

      cheers!