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Airfoil camber and thickness variation algo

Rohan
2017-01-22
2017-01-22
  • Rohan

    Rohan - 2017-01-22

    Hi,

    How does Xflr modify the overall airfoil geometry when camber or t/c values are changed in 'Scale camber and thickness' option. I want to write a matlab code where along with camber and thickness, I can change leading edge radius and trailing edge thickness also.
    Thanks.

     

    Last edit: Rohan 2017-01-22
  • André

    André - 2017-01-22

    The program uses XFoil's functions as a black box. The scaling and camber modification are done in
    XFoil::tcset(double cnew, double tnew)
    The LE mod is in
    XFoil::lerad(double rfac, double blend)
    The TE is set in
    XFoil::tgap(double gapnew, double blend)

     

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