VERSION 1.0 INFO Marauder Segelflugmodell Spannweite: 2 m Gewicht: 2.9 kg RC-Funktionen: Kanal 1: Seitenruder Kanal 2: Hφhenruder Kanal 3: Querruder Copyright 2004 ENDINFO // // ParEditor.Scale=230 // ParEditor.Data1= 2 2 1 1 3 2.8125 3.5674 // ParEditor.Data2=0.5 0.5145 0.5145 0.0912 0.0336 0.2025 0.8 2.1563 // ParEditor.Data3=0 0 0 // ParEditor.Data4=0 0 2 2 -1 -5 // ParEditor.Data5=2 -2 1 -1 0 0 // ParEditor.Data6=1 1 0 0 -2 1 // ParEditor.Data7=15 0.805 AIRPLANE MAIN 1.7 //Mass [Kg] 0.750418 //Roll Inertia Moment Ixx [kg*m^2] 0.189065 //Pitch Inertia Moment Iyy [kg*m^2] 0.93387 //Yaw Inertia Moment Izz [kg*m^2] 0.001247 //Ixz [kg*m^2] -.04 0 0 //dSˆΚ’uX,Y,Z [m] 0.2 //Height of Center of gravity [m] WING //WING1 0.0343 -0.7482 -0.1122 //—ƒˆΚ’uX,Y,Z [m] 1 0 0 //Ex X,Y,Z 0 0.9976 0.0698 //Ey X,Y,Z 1 //polar number 1.5 //span [m] 6 //number of elements AUTOELEMENT 0.6888 //Angle [deg] 0.113 //chord length at the first end [m] 0.23 //chord length at the second end [m] 0.04 //chord length of the flap [m] 0.089 //start position of the flap [m] 0.8115 //end position of the flap [m] -15 //Maximum Angle [deg] 3 //channel //WING2 0.0343 0.7482 -0.1122 //—ƒˆΚ’uX,Y,Z [m] 1 0 0 //Ex X,Y,Z 0 0.9976 -0.0698 //Ey X,Y,Z 1 //polar number 1.5 //span [m] 6 //number of elements AUTOELEMENT 0.6888 //Angle [deg] 0.23 //chord length at the first end [m] 0.113 //chord length at the second end [m] 0.04 //chord length of the flap [m] 0.6885 //start position of the flap [m] 1.411 //end position of the flap [m] 15 //Maximum Angle [deg] 3 //channel //WING3 -0.9 0.0033 -.02 //—ƒˆΚ’uX,Y,Z [m] 1 0 0 //Ex X,Y,Z 0 1 0 //Ey X,Y,Z 2 //polar number 0.76 //span [m] 4 //number of elements AUTOELEMENT -1 //Angle [deg] 0.12 //chord length at the first end [m] 0.12 //chord length at the second end [m] 0.03 //chord length of the flap [m] 0 //start position of the flap [m] 0.76 //end position of the flap [m] 20 //Maximum Angle [deg] 2 //channel //WING4 -0.96 0 -.18 //—ƒˆΚ’uX,Y,Z [m] 0.9397 0 -0.342 //Ex X,Y,Z 0.342 0 0.9397 //Ey X,Y,Z 2 //polar number 0.28 //span [m] 4 //number of elements AUTOELEMENT -1 //Angle [deg] 0.12 //chord length at the first end [m] 0.12 //chord length at the second end [m] 0.06 //chord length of the flap [m] 0 //start position of the flap [m] 0.26 //end position of the flap [m] 25 //Maximum Angle [deg] 1 //channel //WING5 0.02 0 -.04 //—ƒˆΚ’uX,Y,Z [m] 1 0 0 //Ex X,Y,Z 0 0 -1 //Ey X,Y,Z 3 //polar number 0.05 //span [m] 3 //number of elements AUTOELEMENT 0 //Angle [deg] 1.35 //chord length at the first end [m] 1.35 //chord length at the second end [m] 0 //chord length of the flap [m] 0 //start position of the flap [m] 0 //end position of the flap [m] 0 //Maximum Angle [deg] 0 //channel POLAR //POLAR1 19 //ƒf[ƒ^” -180 0 0.03 0 //Œ}Šp(deg),CL,CD,CM -170 0.63 0.1 0 //Œ}Šp(deg),CL,CD,CM -90 0 1.2 0.3 //Œ}Šp(deg),CL,CD,CM -50 -0.3 0.96 0.21 //Œ}Šp(deg),CL,CD,CM -20 -0.46 0.46 0.1 //Œ}Šp(deg),CL,CD,CM -14 -0.55 0.19 0.07 //Œ}Šp(deg),CL,CD,CM -10 -0.54 0.08 0.05 //Œ}Šp(deg),CL,CD,CM -8 -0.55 0.045 0 //Œ}Šp(deg),CL,CD,CM -6 -0.45 0.025 -0.035 //Œ}Šp(deg),CL,CD,CM 0 0.2 0.02 -0.06 //Œ}Šp(deg),CL,CD,CM 7 0.9 0.02 -0.03 //Œ}Šp(deg),CL,CD,CM 13.5 1 0.05 0 //Œ}Šp(deg),CL,CD,CM 14 0.9 0.12 -0.08 //Œ}Šp(deg),CL,CD,CM 17 0.85 0.2 -0.1 //Œ}Šp(deg),CL,CD,CM 22 0.87 0.46 -0.12 //Œ}Šp(deg),CL,CD,CM 50 0.6 0.96 -0.21 //Œ}Šp(deg),CL,CD,CM 90 0.1 1.2 -0.3 //Œ}Šp(deg),CL,CD,CM 170 -0.63 0.1 0 //Œ}Šp(deg),CL,CD,CM 180 0 0.03 0 //Œ}Šp(deg),CL,CD,CM -8 //angle of attack lower flow separation [deg] 13.5 //angle of attack upper flow separation [deg] 1 //flow separation hysteresis [deg] //POLAR2 18 //ƒf[ƒ^” -180 0 0.03 0 //Œ}Šp(deg),CL,CD,CM -170 0.63 0.1 0 //Œ}Šp(deg),CL,CD,CM -90 0 1.2 0.3 //Œ}Šp(deg),CL,CD,CM -50 -0.45 0.96 0.21 //Œ}Šp(deg),CL,CD,CM -20 -0.72 0.46 0.12 //Œ}Šp(deg),CL,CD,CM -12 -0.7 0.19 0.1 //Œ}Šp(deg),CL,CD,CM -10 -0.82 0.08 0 //Œ}Šp(deg),CL,CD,CM -8.2 -0.79 0.045 0 //Œ}Šp(deg),CL,CD,CM -2.5 -0.34 0.025 0 //Œ}Šp(deg),CL,CD,CM 2.5 0.34 0.025 0 //Œ}Šp(deg),CL,CD,CM 8.2 0.79 0.045 0 //Œ}Šp(deg),CL,CD,CM 10 0.82 0.08 0 //Œ}Šp(deg),CL,CD,CM 12 0.7 0.19 -0.1 //Œ}Šp(deg),CL,CD,CM 20 0.72 0.46 -0.12 //Œ}Šp(deg),CL,CD,CM 50 0.45 0.96 -0.21 //Œ}Šp(deg),CL,CD,CM 90 0 1.2 -0.3 //Œ}Šp(deg),CL,CD,CM 170 -0.63 0.1 0 //Œ}Šp(deg),CL,CD,CM 180 0 0.03 0 //Œ}Šp(deg),CL,CD,CM -10 //angle of attack lower flow separation [deg] 10 //angle of attack upper flow separation [deg] 1 //flow separation hysteresis [deg] //POLAR3 18 //ƒf[ƒ^” -180 0 0.03 0 //Œ}Šp(deg),CL,CD,CM -170 0.63 0.1 0 //Œ}Šp(deg),CL,CD,CM -90 0 1.2 0.3 //Œ}Šp(deg),CL,CD,CM -50 -0.45 0.96 0.21 //Œ}Šp(deg),CL,CD,CM -20 -0.72 0.46 0.12 //Œ}Šp(deg),CL,CD,CM -12 -0.7 0.19 0.1 //Œ}Šp(deg),CL,CD,CM -10 -0.82 0.08 0 //Œ}Šp(deg),CL,CD,CM -8.2 -0.79 0.05 0 //Œ}Šp(deg),CL,CD,CM -2.5 -0.34 0.035 0 //Œ}Šp(deg),CL,CD,CM 2.5 0.34 0.035 0 //Œ}Šp(deg),CL,CD,CM 8.2 0.79 0.05 0 //Œ}Šp(deg),CL,CD,CM 10 0.82 0.08 0 //Œ}Šp(deg),CL,CD,CM 12 0.7 0.19 -0.1 //Œ}Šp(deg),CL,CD,CM 20 0.72 0.46 -0.12 //Œ}Šp(deg),CL,CD,CM 50 0.45 0.96 -0.21 //Œ}Šp(deg),CL,CD,CM 90 0 1.2 -0.3 //Œ}Šp(deg),CL,CD,CM 170 -0.63 0.1 0 //Œ}Šp(deg),CL,CD,CM 180 0 0.03 0 //Œ}Šp(deg),CL,CD,CM -10 //angle of attack lower flow separation [deg] 10 //angle of attack upper flow separation [deg] 1 //flow separation hysteresis [deg] POINT //3D‹«ŠEˆΚ’u //POINT1 0.033 3.452 -0.208 //ƒ|ƒCƒ“ƒgˆΚ’u [m] 1000 //spring constant [N/m] 10 //Viscosity [N*s/m] 100 //breaking load [N] 0.6 //coefficent of friction //POINT2 0.033 -3.452 -0.208 //ƒ|ƒCƒ“ƒgˆΚ’u [m] 1000 //spring constant [N/m] 10 //Viscosity [N*s/m] 100 //breaking load [N] 0.6 //coefficent of friction //POINT3 0.84 0 -0.06 //ƒ|ƒCƒ“ƒgˆΚ’u [m] 1000 //spring constant [N/m] 10 //Viscosity [N*s/m] 100 //breaking load [N] 0.6 //coefficent of friction //POINT4 -2.466 0 -0.7 //ƒ|ƒCƒ“ƒgˆΚ’u [m] 1000 //spring constant [N/m] 10 //Viscosity [N*s/m] 70 //breaking load [N] 0.6 //coefficent of friction //POINT5 -2.3 0 -0.04 //ƒ|ƒCƒ“ƒgˆΚ’u [m] 1000 //spring constant [N/m] 10 //Viscosity [N*s/m] 70 //breaking load [N] 0.6 //coefficent of friction WHEEL //ŽΤ—Φ //WHEEL1 0.033 3.452 -0.18 //ŽΤ—ΦˆΚ’u [m] 100 //spring constant [N/m] 40 //Viscosity [N*s/m] 8330 //breaking load [N] 0 1 0 //ŽΤŽ²ƒxƒNƒgƒ‹ [X,Y,Z] 0.2 //coefficient of friction trace direction 0.7 //coeff. of fric. transverse direction 0 //channel 0 //Maximum Angle [deg] //WHEEL2 0.033 -3.452 -0.18 //ŽΤ—ΦˆΚ’u [m] 100 //spring constant [N/m] 40 //Viscosity [N*s/m] 8330 //breaking load [N] 0 -1 0 //ŽΤŽ²ƒxƒNƒgƒ‹ [X,Y,Z] 0.2 //coefficient of friction trace direction 0.7 //coeff. of fric. transverse direction 0 //channel 0 //Maximum Angle [deg] //WHEEL3
0.233 0 -0.18 //ŽΤ—ΦˆΚ’u [m] 100 //spring constant [N/m] 20 //Viscosity [N*s/m] 8330 //breaking load [N] 0 1 0 //ŽΤŽ²ƒxƒNƒgƒ‹ [X,Y,Z] 0.2 //coefficient of friction trace direction 0.7 //coeff. of fric. transverse direction 0 //channel 0 //Maximum Angle [deg] HOOK 0.144 0 0.154 //ƒtƒbƒNˆΚ’uX,Y,Z [m]