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

Question asked by Tan TS on Mar 10, 2008
Latest reply on May 9, 2008 by Anthony Botting
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?