0,0 → 1,113 |
1 1:Type(-) Type[1=Helicopter] ParDesigner Ver0.8 |
|
4.0 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 |
0.05 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 |
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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 |
|
-0.2 1:PosX(m) X Position |
-0.2 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 |
|
-0.2 1:PosX(m) X Position |
0.2 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 |
|
0.5 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 |
|
-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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