adjusting aircraft parameters

[marco...zz]

hi all, what are the lines in the parameter file for adjusting weight, power etc etc so that i can make a model more like my own ?

Many thanks in advance...

[shinichio nishiya]

Hi,
This is my model LiteMoth's par-file.
And I wrote an article about par-file arrangement.
Visit here.

This is for airplanes.
I hope it would be a help for you.

Shinichiro Nishiya
Aomori city, Japan



0 --------- 1:Type(-) -------- Airplane:0 / LiteMoth 2001.10.17 (original from KOKENKI by TOKUSASU)
6 --------- 2:Tmax(N) -------Maximum Thrust / 2001.10.19 reduced the power from [8] to [6]
0.30 ---- 3:Drmax(rad) ---Maximum Rudder Throw
0.10 ---- 4:Demax(rad) --Maxmum Elevator Throw
0.003 -- 5:Damax(rad) --Maximum Ailrons Throw / NO AILERON:INPUT [0]
1.4 ------ 6:CLmax(-) -----Maximum Lift Coefficient
-0.45 --- 7:CLmin(-) -------MInimum Lift Coefficient
3.7 ------ 8:CLa(/rad) ----- Lift Gradient
10 ------ 9:CLaSt(/rad)---Lift Gradient in Stall
0.02 ---- 10:CDw0(-) ------Drag Coefficient of Wing
0.04 ---- 11:CDb(-) ---------Drag Coefficient of Fuselage
0.2 ------ 12:mug(-) -------- Friction Coefficient of Wheel
0.69 ---- 13:dCDSt(-) -----Rise of Drag Coefficient in Stall
0.00 ---- 14:CM(-) -----------Moment Coefficient
0.04 ---- 15:alpha0(rad) --Wing Attack Angle
1.48 ---- 16:b(m) ------------Wing Span
0.23 ---- 17:c(m) ------------ Wing Chord
0.10 ---- 18:hce(m) -------- Equivalent Center of Gravity
0.9 ------ 19:m(Kg) --------- Mass
0.18 ---- 20:Ixx(Kg*m^2) -Yaw Inertia Moment
0.024 -- 21:Iyy(Kg*m^2) -Pitch Inertia Moment
0.010 -- 22:Izz(Kg*m^2) -Roll Inertia Moment
0.05 ---- 23:She(m^2) -----Effective Area of Stab
0.03 ---- 24:Sfe(m^2) ------Effective Area of Fin
0.70 ---- 25:Lt(m) -----------Tail Moment Arm
0.004 -- 26:VForm(-) ------Effect of Dihedral Angle

[marco...zz]

great thanks for that