0        1:Type(-)      Type[0=Plane] ParDesigner Ver0.8 CarbonFalcon from Tzagi
3.800    2:Tmax(N)      Maximum Thrust
0.0000   3:Drmax(rad)   Maximun Rudder Angle
0.0500   4:Demax(rad)   Maxmim Elevator Angle
0.0025   5:Damax(rad)   Maximim Aileron Angle
1.100    6:CLmax(-)     Maximum Lift Coefficient
-1.500   7:CLmin(-)     Minimum Lift Coefficient
6.200    8:CLa(/rad)    Lift Gradient
6.000    9:CLaSt(/rad)  Lift Gradient in Stall
0.0180   10:CDw(-)      Drag Coefficient of Wing
0.0200   11:CDb(-)      Drag Coefficient of Fuselage
0.4000   12:mug(-)      Friction Coefficient of Wheels
0.2600   13:dCDSt(-)    Rise of Drag Coefficient in Stall
-0.0400  14:CM(-)       Moment Coefficient
0.04000  15:alpha0(rad) Wing Angle
1.2000   16:b(m)        Wing Span
0.3000   17:c(m)        Wing Chord
0.12000  18:hce(m)      Equivalent Center of Gravity
0.7000   19:m(Kg)       Mass
0.1100   20:Izz(Kg*m^2) Yaw Inertia Moment
0.0280   21:Iyy(Kg*m^2) Pitch Inertia Moment
0.0200   22:Ixx(Kg*m^2) Roll Inertia Moment
0.0500   23:She(m^2)    Effective Area of Stab
0.0400   24:Sfe(m^2)    Effective Area of fin
1.000    25:Lt(m)       Tail Moment Arm
0.01000  26:VForm(-)    Effect of Dihedral Angle