#============ Name Ultralight Sailplane End #============ Units L 1.0 ft T 1.0 s F 1.0 lb End #============ Constant # g rho_SL V_sound 32.18 0.002378 1115.0 End #============ Reference # Sref Cref Bref 125.0 3.0 49.2 # # Xmom Ymom Zmom -0.40 0.0 0.0 -0.40 0.0 0.0 -0.40 0.0 0.0 End #============ Joint # Nbeam1 Nbeam2 t1 t2 4 1 0.0 0.0 4 3 11.4 1.0 3 2 6.0 0.0 End #============ Ground # Nbeam t Kground ! 1 0.0 0 ! 2 0.0 0 ! 3 0.0 0 4 0.0 0 End #====================== Weight # Nbeam t Xp Yp Zp Mg CDA Vol Hx Hy Hz * 1. 1. 1. 1. 1. 1. 1. 1. 1. 1. # # different size pilots ! 4 -1.83 -2.83 0.0 0.0 225.0 0.0 0.0 0.0 0.0 0.0 4 -1.83 -2.83 0.0 0.0 160.0 0.0 0.0 0.0 0.0 0.0 ! 4 -1.83 -2.83 0.0 0.0 140.0 0.0 0.0 0.0 0.0 0.0 4 0.00 0.00 0.0 -1.0 4.0 0.0 0.0 0.0 0.0 0.0 4 0.00 0.00 0.0 +0.5 15.0 0.0 0.0 0.0 0.0 0.0 4 0.00 1.50 0.0 0.0 6.0 0.0 0.0 0.0 0.0 0.0 # # tail ballast ! 4 11.40 11.40 0.0 0.0 15.0 0.0 0.0 0.0 0.0 0.0 4 11.40 11.40 0.0 0.0 5.0 0.0 0.0 0.0 0.0 0.0 End #====================== Sensor # KS Nb t Xp Yp Zp Vx Vy Vz Ax Ay Az * 1. 1. 1. 0.0 1. 1. 1. 1. 1. 1. * 1. 1. 1. 0.04 1. 1. 1. 1. 1. 1. 1 1 -24.6 -1.40 -24.6 24.6 1.0 0.0 0.0 0.0 0.0 1.0 2 1 -19.7 -1.40 -19.7 19.7 1.0 0.0 0.0 0.0 0.0 1.0 3 1 -8.01 -1.40 -8.0 8.0 1.0 0.0 0.0 0.0 0.0 1.0 4 1 0.0 -1.40 0.0 0.0 1.0 0.0 0.0 0.0 0.0 1.0 5 1 8.01 -1.40 8.0 8.0 1.0 0.0 0.0 0.0 0.0 1.0 6 1 19.7 -1.40 19.7 19.7 1.0 0.0 0.0 0.0 0.0 1.0 7 1 24.6 -1.40 24.6 24.6 1.0 0.0 0.0 0.0 0.0 1.0 8 4 0.0 0.0 0.0 0.0 1.0 0.0 0.0 0.0 0.0 1.0 End #============ Engine # KPeng IEtyp Nbeam t Xp Yp Zp Tx Ty Tz dFdPe dMdPe Rdisk Omega cdA ! 1 1 4 1.0 -6.975 0. 0. -1. 0. -.1 1.0 1.0 3.0 100. 0.0 1 0 4 1.0 -6.975 0. 0. -1. 0. -.1 1.0 0.01 0.0 100. 0.0 End #============ Beam 1 Wing t x y z chord twist Xax * 1. 1. 1. 0.0412 1. 1. 0.4 0.00000 0.00000 0.00000 0.00000 3.00000 1.00000 1.00000 1.81241 -0.06198 1.81241 1.81241 2.99672 1.00000 1.00000 3.61364 -0.12086 3.61364 3.61364 2.98667 1.00000 1.00000 5.39259 -0.17600 5.39259 5.39259 2.96923 1.00000 1.00000 7.13829 -0.22665 7.13829 7.13829 2.94344 1.00000 1.00000 8.83999 -0.27193 8.83999 8.83999 2.90807 1.00000 1.00000 10.48718 -0.31090 10.48718 10.48718 2.86169 1.00000 1.00000 12.06972 -0.34263 12.06972 12.06972 2.80287 1.00000 1.00000 13.57784 -0.36626 13.57784 13.57784 2.73027 1.00000 1.00000 15.00225 -0.38102 15.00225 15.00225 2.64283 1.00000 1.00000 16.33417 -0.38637 16.33417 16.33417 2.53992 1.00000 1.00000 17.56538 -0.38202 17.56538 17.56538 2.42157 1.00000 1.00000 18.68830 -0.36806 18.68830 18.68830 2.28864 1.00000 1.00000 19.69599 -0.34502 19.69599 19.69599 2.14306 1.00000 1.00000 20.58225 -0.31276 20.58225 20.58225 1.99172 1.00000 1.00000 21.34162 -0.27222 21.34162 21.34162 1.84220 1.00000 1.00000 21.96941 -0.22670 21.96941 21.96941 1.70013 1.00000 1.00000 22.46175 -0.18081 22.46175 22.46175 1.57303 1.00000 1.00000 22.81560 -0.14051 22.81560 22.81560 1.47041 1.00000 1.00000 23.02879 -0.11245 23.02879 23.02879 1.40278 1.00000 1.00000 23.10000 -0.10233 23.10000 23.10000 1.37903 1.00000 1.00000 ! 23.10000 -0.10233 23.10000 23.10000 1.37903 1.00000 1.00000 23.17427 -0.09133 23.17427 23.17427 1.35359 1.00000 1.00000 23.38238 -0.05779 23.38238 23.38238 1.27810 1.00000 1.00000 23.68311 -0.00043 23.68311 23.68311 1.15535 1.00000 1.00000 24.01689 0.08177 24.01689 24.01689 0.99057 1.00000 1.00000 24.31762 0.18842 24.31762 24.31762 0.79199 1.00000 1.00000 24.60000 0.31657 24.60000 24.60000 0.55000 1.00000 1.00000 ! 24.60000 0.46037 24.60000 24.60000 0.34120 1.00000 1.00000 t Cshell Nshell Atshell * 1. 0.35 0.09 0.0001 0.00000 3.00000 3.00000 3.00000 1.81241 2.99672 2.99672 2.99672 3.61364 2.98667 2.98667 2.98667 5.39259 2.96923 2.96923 2.96923 7.13829 2.94344 2.94344 2.94344 8.83999 2.90807 2.90807 2.90807 10.48718 2.86169 2.86169 2.86169 12.06972 2.80287 2.80287 2.80287 13.57784 2.73027 2.73027 2.73027 15.00225 2.64283 2.64283 2.64283 16.33417 2.53992 2.53992 2.53992 17.56538 2.42157 2.42157 2.42157 18.68830 2.28864 2.28864 2.28864 19.69599 2.14306 2.14306 2.14306 20.58225 1.99172 1.99172 1.99172 21.34162 1.84220 1.84220 1.84220 21.96941 1.70013 1.70013 1.70013 22.46175 1.57303 1.57303 1.57303 22.81560 1.47041 1.47041 1.47041 23.02879 1.40278 1.40278 1.40278 23.10000 1.37903 1.37903 1.37903 ! 23.10000 1.37903 1.37903 1.37903 23.17427 1.35359 1.35359 1.35359 23.38238 1.27810 1.27810 1.27810 23.68311 1.15535 1.15535 1.15535 24.01689 0.99057 0.99057 0.99057 24.31762 0.79199 0.79199 0.79199 24.60000 0.55000 0.55000 0.55000 ! 24.60000 0.34120 0.34120 0.34120 t mg mgnn EIcc EInn GJ EIcs EIsn * 1. 0.9 0.9 1.0E5 5.0E6 1.0E5 0. 0. -24.6 1.2 1.2 0.005 0.1 0.05 -0.005 -0.1 -24.0 1.21 1.21 0.006 0.105 0.0505 -0.006 -0.105 -20.0 1.5 1.5 0.04 0.20 0.12 -0.04 -0.20 -10.0 3.0 3.0 0.65 0.75 0.5 -0.65 -0.75 0.0 5.0 5.0 2.0 2.0 1.0 -2.0 -2.0 0.0 5.0 5.0 2.0 2.0 1.0 2.0 2.0 10.0 3.0 3.0 0.65 0.75 0.5 0.65 0.75 20.0 1.5 1.5 0.04 0.20 0.12 0.04 0.20 24.0 1.21 1.21 0.006 0.105 0.0505 0.006 0.105 24.6 1.2 1.2 0.005 0.1 0.05 0.005 0.1 t Ccg * 1. 0. 0.0 1.0 10.0 1.0 20.0 1.0 24.0 1.0 24.6 1.0 t alpha * 1. 1. 0.0 4.0 10.0 4.0 20.0 4.0 24.0 4.0 24.6 4.0 t CLmax CLmin Cdf Cdp * 1. 1. 1. 1. 1. 0.0 2.1 -1.0 0.006 0.004 10.0 2.1 -1.0 0.0064 0.0044 20.0 2.1 -1.0 0.0068 0.0048 24.0 2.1 -1.0 0.009 0.006 24.6 2.1 -1.0 0.012 0.008 # # alternative flap schedule ! t dCLdF4 dCLdF1 dCMdF4 dCMdF1 Cm !* 1. 1. 1. -0.25 -0.25 1.0 ! -24.6 0.0 0.0 0.0 0.0 -0.19 ! -24.0 0.0 0.0 0.0 0.0 -0.19 ! -24.0 0.04 0.03 0.04 0.03 -0.19 ! -16.0 0.04 0.03 0.04 0.03 -0.19 ! -16.0 0.06 0.02 0.06 0.02 -0.19 ! -8.01 0.06 0.02 0.06 0.02 -0.19 ! -8.01 0.07 0.01 0.07 0.01 -0.19 ! 0.0 0.07 0.01 0.07 0.01 -0.19 ! 0.0 0.07 -0.03 0.07 -0.03 -0.19 ! 8.01 0.07 -0.03 0.07 -0.03 -0.19 ! 8.01 0.06 -0.06 0.06 -0.06 -0.19 ! 16.0 0.06 -0.06 0.06 -0.06 -0.19 ! 16.0 0.04 -0.09 0.04 -0.09 -0.19 ! 24.0 0.04 -0.09 0.04 -0.09 -0.19 ! 24.0 0.0 0.0 0.0 0.0 -0.19 ! 24.6 0.0 0.0 0.0 0.0 -0.19 t dCLdF4 dCLdF1 dCMdF4 dCMdF1 Cm * 1. 1. 1. -0.25 -0.25 1.0 -24.6 0.0 0.0 0.0 0.0 -0.19 -24.0 0.0 0.0 0.0 0.0 -0.19 -24.0 0.04 0.06 0.04 0.06 -0.19 -16.0 0.04 0.06 0.04 0.06 -0.19 -16.0 0.06 0.04 0.06 0.04 -0.19 -8.01 0.06 0.04 0.06 0.04 -0.19 -8.01 0.07 0.02 0.07 0.02 -0.19 0.0 0.07 0.02 0.07 0.02 -0.19 0.0 0.07 -0.02 0.07 -0.02 -0.19 8.01 0.07 -0.02 0.07 -0.02 -0.19 8.01 0.06 -0.04 0.06 -0.04 -0.19 16.0 0.06 -0.04 0.06 -0.04 -0.19 16.0 0.04 -0.06 0.04 -0.06 -0.19 24.0 0.04 -0.06 0.04 -0.06 -0.19 24.0 0.0 0.0 0.0 0.0 -0.19 24.6 0.0 0.0 0.0 0.0 -0.19 End #=========== Beam 2 Horizontal Stab t x y z chord twist Xax + 0. 11.4 0. 5.0 0. -4. 0. * 1. 1. 1. 1. 1. 1. 0.4 0.00000 0.24000 0.00000 0.00000 1.40000 0.00000 1.0000 0.78316 0.24254 0.78316 0.00000 1.39275 0.00000 1.0000 1.55291 0.25036 1.55291 0.00000 1.37041 0.00000 1.0000 2.29610 0.26404 2.29610 0.00000 1.33132 0.00000 1.0000 3.00000 0.28443 3.00000 0.00000 1.27306 0.00000 1.0000 3.65257 0.31244 3.65257 0.00000 1.19302 0.00000 1.0000 4.24264 0.34888 4.24264 0.00000 1.08898 0.00000 1.0000 4.76012 0.39665 4.76012 0.00000 0.96666 0.00000 1.0000 5.19615 0.45761 5.19615 0.00000 0.83173 0.00000 1.0000 5.54328 0.53104 5.54328 0.00000 0.68599 0.00000 1.0000 5.79556 0.61538 5.79556 0.00000 0.53243 0.00000 1.0000 6.00000 0.70823 6.00000 0.00000 0.37513 0.00000 1.0000 ! 6.00000 0.80662 6.00000 0.00000 0.21892 0.00000 1.0000 t mg mgnn * 1. 1.2 1.0 0.0 0.80 0.10 3.0 0.55 0.04 6.0 0.40 0.015 t CLmax CLmin Cm dCLdF2 dCMdF2 * 1. 1. 1. 1. 1. 1. 0.0 1.2 -1.2 0.0 0.05 -0.03 6.0 1.2 -1.2 0.0 0.05 -0.03 t EIcc EInn GJ * 1.0 1.0E4 1.0E5 4.0E4 0.0 1.0 1.0 1.0 3.0 0.4 0.6 0.8 6.0 0.2 0.2 0.6 End #=========== Beam 3 2 Vertical Stab t x z chord Xax + 1. 11.4 0.0 0. 0.0 * 1. 1. 1. 1. 1. 0.0000 0.40 0.0 3.0 0.80 2.5000 0.40 2.5 2.25 0.7333 4.0000 0.40 4.0 1.8 0.6667 5.0000 0.40 5.0 1.5 0.60 t mg mgnn + 1. 0.0 0.0 * 1. 1. 1. 0.0000 1.5 0.20 2.5000 1.25 0.12 4.0000 1.1 0.07 5.0000 1.0 0.04 t CLmax CLmin Cm dCLdF3 dCMdF3 + 1. 0.0 0.0 0. 0. 0. * 1. 1. 1. 1. 1. 1. 0.0 1.2 -1.2 0.0 -0.05 0.03 5.0 1.2 -1.2 0.0 -0.05 0.03 t EIcc EInn GJ * 1.0 3.0E4 3.0E5 3.0E4 0.0 1.0 1.0 1.0 2.5 0.9 0.7 0.8 5.0 0.8 0.4 0.6 End #=========== Beam 4 Fuselage t x radius mg * 1.0 1.0 1.0 1.5 -7.5000 -7.5000 0.07680 0.07680 -7.4797 -7.4797 0.09301 0.09301 -7.4000 -7.4000 0.15360 0.15360 -7.2751 -7.2751 0.23941 0.23941 -7.0000 -7.0000 0.38981 0.38981 -6.5866 -6.5866 0.54262 0.54262 -6.0000 -6.0000 0.70361 0.70361 -5.0000 -5.0000 0.92558 0.92558 -4.0000 -4.0000 1.05922 1.05922 -2.0000 -2.0000 1.17204 1.17204 0.0000 0.0000 1.09189 1.09189 3.0000 3.0000 0.70182 0.70182 5.0000 5.0000 0.49062 0.49062 8.0000 8.0000 0.29618 0.29618 11.4000 11.4000 0.19990 0.19990 t EIcc EInn GJ * 1.0 1.0E5 1.0E5 1.0E5 -7.5 0.6 0.6 0.3 -6.0 0.9 0.9 0.5 -3.0 1.5 1.5 0.8 0.0 1.5 1.5 0.8 6.0 0.9 0.9 0.6 11.4 0.4 0.4 0.4 t Cdf Cdp * 1. 1. 1. -7.5 0.003 0.3 -6.0 0.003 0.3 -3.0 0.003 0.3 0.0 0.003 0.3 6.0 0.003 0.3 11.4 0.003 0.3 End