0        1:Type(-)      Type[0=Plane] ParDesigner Ver0.8
38       2:Tmax(N)      Maximum Thrust
0.07     3:Drmax(rad)   Maximun Rudder Angle
0.1      4:Demax(rad)   Maxmim Elevator Angle
0.00065  5:Damax(rad)   Maximim Aileron Angle
1        6:CLmax(-)     Maximum Lift Coefficient
-1       7:CLmin(-)     Minimum Lift Coefficient
5.8      8:CLa(/rad)    Lift Gradient
14       9:CLaSt(/rad)  Lift Gradient in Stall
0.012    10:CDw(-)      Drag Coefficient of Wing
0.018    11:CDb(-)      Drag Coefficient of Fuselage
0.4      12:mug(-)      Friction Coefficient of Wheels
0.76     13:dCDSt(-)    Rise of Drag Coefficient in Stall
0.0      14:CM(-)       Moment Coefficient
0.034    15:alpha0(rad) Wing Angle
3.2      16:b(m)        Wing Span
0.38     17:c(m)        Wing Chord
0.085    18:hce(m)      Equivalent Center of Gravity
6        19:m(Kg)       Mass
0.4      20:Izz(Kg*m^2) Yaw Inertia Moment
0.32     21:Iyy(Kg*m^2) Pitch Inertia Moment
0.22     22:Ixx(Kg*m^2) Roll Inertia Moment
0.05     23:She(m^2)    Effective Area of Stab
0.04     24:Sfe(m^2)    Effective Area of fin
1        25:Lt(m)       Tail Moment Arm
0.001    26:VForm(-)    Effect of Dihedral Angle
0.20     27: Flugzeughöhe
1          28 : Beleuchtung ein
