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  • Moderator

    Use a XFLR

  • Hi,

    the static margin of longitudinal stability can be calculated from

    static margin = (AC-CP) / c

    AC is the position of the aerodynamic center, CP is the Center of pressure, and c typically is the mean aerodynamic chord.

    All three are not so easy to calculate. You may want to use a free tool such as

    Aeolus Aero Sketch Pad https://www.aeolus-aero.com/software/

    which does the work for you.

    Best regards,

    Uwe

    Products & Services
    Advanced aircraft design software for more efficient aircraft.
  • https://www.facebook.com/Airloads

    Airloads_Marketplace
    Airloads_Marketplace. 2 likes. Simple and efficient systems.
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