Heli .par file English I think =)

[Wyu]

I'm not shire is this a .par file some one was looking for in english?




1 1:Type(-) Type[1=Helicopter] ParDesigner Ver0.8

7.5 2:m(Kg) Mass
0.55 3:Izz(Kg*m^2) Yaw Inertia Moment
0.75 4:Iyy(Kg*m^2) Pitch Inertia Moment
0.75 5:Ixx(Kg*m^2) Roll Inertia Moment
2.2 6:Ct(-) Friction for Rotate(Yaw)

10 7:ExpE(%) Elevator Expoential Ratio
10 8:ExpA(%) Aileron Expoential Ratio
15 9:ExpR(%) Rudder Expoential Ratio
0 10:ExpP(%) Collective Pitch Expoential Ratio

0.65 11:R(m) Length of Main Blade
0.04 12:S(m^2) Area of Main Blades
1800 13:N(rmp) Revolution of Main Rotor
0.1 14:Pmax(rad) Collective Pitch
0.003 15:Emax(rad) Elevator Cyclic Pitch
0.004 16:Amax(rad) Aileron Cyclic Pitch
0.0 17:Hm(m) Position of Main Rotor from Center of Gravity
0.001 18:fhorzd(-) Effect of Side Wind

0.18 19:Rt(m) Length of Tail Blade
0.02 20:St(m^2) Area of Tail Blades
5950 21:Nt(rmp) Revolution of Tail Rotor
0.075 22:Rmax(rad) Maximum Pitch of Tail Braid
0.009 23:at0(rad) Refarence Pitch of Tail Braid
0.9 24:Lt(m) Position of Tail Rotor from Center of Gravity
0.25 25:fhorzdh(-) Yow Stabilization

0.05 26:kG(s) Sensitivity of Gyroscope
80 27:mG(%) Mixing of Gyroscope

6.2 28:CLa(/rad) Gradient of Lift Coefficient
0.8 29:CLmax(-) Maximum Lift Coefficient
-0.6 30:CLmin(-) Minimum Lift Coefficient
0.02 31:Cd0(-) Profile Drag Coefficient
0.02 32:kCdi(-) Rise Rate of Indused Drag Coefficient
0.3 33:CDb(-) Drag Coefficient of Fuselage

5 34:nb(-)

0.3 1:PosX(m)
0.3 2:PosY(m)
-0.20 3:PosZ(m)
1.0 4:muh(-)
4000 5:h(N/m)
10 6:muv(-)
1200 7:fmax(N)

0.3 1:PosX(m)
-0.3 2:PosY(m)
-0.20 3:PosZ(m)
1.0 4:muh(-)
4000 5:h(N/m)
10 6:muv(-)
1200 7:fmax(N)

-0.3 1:PosX(m)
-0.3 2:PosY(m)
-0.20 3:PosZ(m)
1.0 4:muh(-)
4000 5:h(N/m)
10 6:muv(-)
1200 7:fmax(N)

-0.3 1:PosX(m)
0.3 2:PosY(m)
-0.20 3:PosZ(m)
1.0 4:muh(-)
4000 5:h(N/m)
10 6:muv(-)
1200 7:fmax(N)

-1.4 1:PosX(m)
0.0 2:PosY(m)
0.038 3:PosZ(m)
2 4:muh(-)
2500 5:h(N/m)
10 6:muv(-)
600 7:fmax(N)

[Scarz]

thanks