[PR]ﾃﾚﾋﾞ番組表
今夜の番組ﾁｪｯｸ

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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


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