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Ignore whitespace Rev 795 → Rev 796

/FMS-Modelle/Hexa/Hexa.par
0,0 → 1,113
1 1:Type(-) Type[1=Helicopter] ParDesigner Ver0.8
 
5 2:m(Kg) Mass
0.3 3:Izz(Kg*m^2) Yaw Inertia Moment
0.3 4:Iyy(Kg*m^2) Pitch Inertia Moment
0.3 5:Ixx(Kg*m^2) Roll Inertia Moment
1.8 6:Ct(-) Friction for Rotate(Yaw)
 
40 7:ExpE(%) Elevator Expoential Ratio
40 8:ExpA(%) Aileron Expoential Ratio
0 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
1900 13:N(rmp) Revolution of Main Rotor
0.08 14:Pmax(rad) Collective Pitch
0.008 15:Emax(rad) Elevator Cyclic Pitch
0.008 16:Amax(rad) Aileron Cyclic Pitch
0 17:Hm(m) Position of Main Rotor from Center of Gravity
0.01 18:fhorzd(-) Effect of Side Wind
 
0.18 19:Rt(m) Length of Tail Blade
0.020 20:St(m^2) Area of Tail Blades
4800 21:Nt(rmp) Revolution of Tail Rotor
0.12 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
0.0 25:fhorzdh(-) Yow Stabilization
 
0.1 26:kG(s) Sensitivity of Gyroscope
0 27:mG(%) Mixing of Gyroscope
 
6.0 28:CLa(/rad) Gradient of Lift Coefficient
0.8 29:CLmax(-) Maximum Lift Coefficient
0.0 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
 
8 34:nb(-) Points of fuselage
 
0.3 1:PosX(m) X Position
0.3 2:PosY(m) Y Position
-0.15 3:PosZ(m) X Position
2 4:muh(-) Horizontal Friction Coefficient
1000 5:h(N/m) Rigidity
10 6:muv(-) Vertical Friction Coefficient
900 7:fmax(N) Strength
 
0.3 1:PosX(m) X Position
-0.3 2:PosY(m) Y Position
-0.15 3:PosZ(m) X Position
2 4:muh(-) Horizontal Friction Coefficient
1000 5:h(N/m) Rigidity
10 6:muv(-) Vertical Friction Coefficient
900 7:fmax(N) Strength
 
-0.3 1:PosX(m) X Position
-0.3 2:PosY(m) Y Position
-0.15 3:PosZ(m) X Position
2 4:muh(-) Horizontal Friction Coefficient
1000 5:h(N/m) Rigidity
10 6:muv(-) Vertical Friction Coefficient
900 7:fmax(N) Strength
 
-0.3 1:PosX(m) X Position
0.3 2:PosY(m) Y Position
-0.15 3:PosZ(m) X Position
2 4:muh(-) Horizontal Friction Coefficient
1000 5:h(N/m) Rigidity
10 6:muv(-) Vertical Friction Coefficient
900 7:fmax(N) Strength
 
0 1:PosX(m) X Position
0 2:PosY(m) Y Position
0.5 3:PosZ(m) X Position
1 4:muh(-) Horizontal Friction Coefficient
2500 5:h(N/m) Rigidity
10 6:muv(-) Vertical Friction Coefficient
6 7:fmax(N) Strength
 
-0.5 1:PosX(m) X Position
0.5 2:PosY(m) Y Position
0.1 3:PosZ(m) X Position
1 4:muh(-) Horizontal Friction Coefficient
2500 5:h(N/m) Rigidity
10 6:muv(-) Vertical Friction Coefficient
6 7:fmax(N) Strength
 
-0.5 1:PosX(m) X Position
-0.5 2:PosY(m) Y Position
0.1 3:PosZ(m) X Position
1 4:muh(-) Horizontal Friction Coefficient
2500 5:h(N/m) Rigidity
10 6:muv(-) Vertical Friction Coefficient
6 7:fmax(N) Strength
 
0.5 1:PosX(m) X Position
-0.5 2:PosY(m) Y Position
0.1 3:PosZ(m) X Position
1 4:muh(-) Horizontal Friction Coefficient
2500 5:h(N/m) Rigidity
10 6:muv(-) Vertical Friction Coefficient
6 7:fmax(N) Strength
 
0.5 1:PosX(m) X Position
0.5 2:PosY(m) Y Position
0.1 3:PosZ(m) X Position
1 4:muh(-) Horizontal Friction Coefficient
2500 5:h(N/m) Rigidity
10 6:muv(-) Vertical Friction Coefficient
6 7:fmax(N) Strength
Property changes:
Added: svn:executable
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