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Rev | Author | Line No. | Line |
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796 | - | 1 | 1 1:Type(-) Type[1=Helicopter] ParDesigner Ver0.8 |
2 | |||
3 | 5 2:m(Kg) Mass |
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4 | 0.3 3:Izz(Kg*m^2) Yaw Inertia Moment |
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5 | 0.3 4:Iyy(Kg*m^2) Pitch Inertia Moment |
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6 | 0.3 5:Ixx(Kg*m^2) Roll Inertia Moment |
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7 | 1.8 6:Ct(-) Friction for Rotate(Yaw) |
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8 | |||
9 | 40 7:ExpE(%) Elevator Expoential Ratio |
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10 | 40 8:ExpA(%) Aileron Expoential Ratio |
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11 | |||
12 | |||
13 | |||
14 | 0.65 11:R(m) Length of Main Blade |
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15 | 0.04 12:S(m^2) Area of Main Blades |
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16 | 1900 13:N(rmp) Revolution of Main Rotor |
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17 | 0.08 14:Pmax(rad) Collective Pitch |
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18 | 0.008 15:Emax(rad) Elevator Cyclic Pitch |
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19 | 0.008 16:Amax(rad) Aileron Cyclic Pitch |
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20 | |||
21 | 0.01 18:fhorzd(-) Effect of Side Wind |
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22 | |||
23 | 0.18 19:Rt(m) Length of Tail Blade |
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24 | 0.020 20:St(m^2) Area of Tail Blades |
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25 | 4800 21:Nt(rmp) Revolution of Tail Rotor |
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26 | 0.12 22:Rmax(rad) Maximum Pitch of Tail Braid |
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27 | 0.009 23:at0(rad) Refarence Pitch of Tail Braid |
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28 | 0.9 24:Lt(m) Position of Tail Rotor from Center of Gravity |
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29 | 0.0 25:fhorzdh(-) Yow Stabilization |
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30 | |||
31 | 0.1 26:kG(s) Sensitivity of Gyroscope |
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32 | |||
33 | |||
34 | 6.0 28:CLa(/rad) Gradient of Lift Coefficient |
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35 | 0.8 29:CLmax(-) Maximum Lift Coefficient |
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36 | 0.0 30:CLmin(-) Minimum Lift Coefficient |
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37 | 0.02 31:Cd0(-) Profile Drag Coefficient |
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38 | 0.02 32:kCdi(-) Rise Rate of Indused Drag Coefficient |
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39 | 0.3 33:CDb(-) Drag Coefficient of Fuselage |
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40 | |||
41 | 8 34:nb(-) Points of fuselage |
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42 | |||
43 | 0.3 1:PosX(m) X Position |
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44 | 0.3 2:PosY(m) Y Position |
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45 | -0.15 3:PosZ(m) X Position |
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46 | 2 4:muh(-) Horizontal Friction Coefficient |
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47 | 1000 5:h(N/m) Rigidity |
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48 | 10 6:muv(-) Vertical Friction Coefficient |
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49 | 900 7:fmax(N) Strength |
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50 | |||
51 | 0.3 1:PosX(m) X Position |
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52 | -0.3 2:PosY(m) Y Position |
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53 | -0.15 3:PosZ(m) X Position |
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54 | 2 4:muh(-) Horizontal Friction Coefficient |
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55 | 1000 5:h(N/m) Rigidity |
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56 | 10 6:muv(-) Vertical Friction Coefficient |
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57 | 900 7:fmax(N) Strength |
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58 | |||
59 | -0.3 1:PosX(m) X Position |
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60 | -0.3 2:PosY(m) Y Position |
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61 | -0.15 3:PosZ(m) X Position |
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62 | 2 4:muh(-) Horizontal Friction Coefficient |
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63 | 1000 5:h(N/m) Rigidity |
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64 | 10 6:muv(-) Vertical Friction Coefficient |
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65 | 900 7:fmax(N) Strength |
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66 | |||
67 | -0.3 1:PosX(m) X Position |
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68 | 0.3 2:PosY(m) Y Position |
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69 | -0.15 3:PosZ(m) X Position |
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70 | 2 4:muh(-) Horizontal Friction Coefficient |
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71 | 1000 5:h(N/m) Rigidity |
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72 | 10 6:muv(-) Vertical Friction Coefficient |
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73 | 900 7:fmax(N) Strength |
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74 | |||
75 | |||
76 | |||
77 | 0.5 3:PosZ(m) X Position |
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78 | 1 4:muh(-) Horizontal Friction Coefficient |
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79 | 2500 5:h(N/m) Rigidity |
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80 | 10 6:muv(-) Vertical Friction Coefficient |
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81 | 6 7:fmax(N) Strength |
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82 | |||
83 | -0.5 1:PosX(m) X Position |
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84 | 0.5 2:PosY(m) Y Position |
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85 | 0.1 3:PosZ(m) X Position |
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86 | 1 4:muh(-) Horizontal Friction Coefficient |
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87 | 2500 5:h(N/m) Rigidity |
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88 | 10 6:muv(-) Vertical Friction Coefficient |
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89 | 6 7:fmax(N) Strength |
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90 | |||
91 | -0.5 1:PosX(m) X Position |
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92 | -0.5 2:PosY(m) Y Position |
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93 | 0.1 3:PosZ(m) X Position |
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94 | 1 4:muh(-) Horizontal Friction Coefficient |
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95 | 2500 5:h(N/m) Rigidity |
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96 | 10 6:muv(-) Vertical Friction Coefficient |
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97 | 6 7:fmax(N) Strength |
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98 | |||
99 | 0.5 1:PosX(m) X Position |
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100 | -0.5 2:PosY(m) Y Position |
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101 | 0.1 3:PosZ(m) X Position |
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102 | 1 4:muh(-) Horizontal Friction Coefficient |
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103 | 2500 5:h(N/m) Rigidity |
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104 | 10 6:muv(-) Vertical Friction Coefficient |
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105 | 6 7:fmax(N) Strength |
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106 | |||
107 | 0.5 1:PosX(m) X Position |
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108 | 0.5 2:PosY(m) Y Position |
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109 | 0.1 3:PosZ(m) X Position |
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110 | 1 4:muh(-) Horizontal Friction Coefficient |
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111 | 2500 5:h(N/m) Rigidity |
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112 | 10 6:muv(-) Vertical Friction Coefficient |
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113 | 6 7:fmax(N) Strength |