#============ Name Daedalus HPA End #============ Units L 1.0 ft T 1.0 s F 1.0 lb End #============ Constant 32.18 0.002378 1115.0 End #============ Reference # Sref Cref Bref 330.0 2.95 112.0 # # Xmom Ymom Zmom 0.0 0.0 0.0 End #============ Strut # Nbeam t Xp Yp Zp Xw Yw Zw dL EAw 1 28. 0.0 28.0 0.35 0.0 0.0 -5.40 0.33 120000.0 1 -28. 0.0 -28.0 0.35 0.0 0.0 -5.40 0.33 120000.0 End #============ Joint # Nbeam1 Nbeam2 t1 t2 5 4 -10.0 2.5 4 1 0.0 0.0 4 2 17.5 0.0 4 3 20.0 0.0 End #============ Ground # Nbeam t Kground 5 -15.6 0 End #====================== Weight # Nbeam t Xp Yp Zp Mg CDA Vol Hx Hy Hz * 1.0 1.0 1.0 1.0 1.0 1.0 1.0 1. 1. 1. ! pilot 5 -13.2 0.0 0.0 -4.0 165.0 0.0 0.0 0.0 0.0 0.0 ! water 5 -13.2 -0.2 0.0 -5.5 12.0 0.0 0.0 0.0 0.0 0.0 ! prop 4 -6.5 -6.5 0.0 0.0 3.0 0.2 0.0 0.0 0.0 0.0 ! top gearbox 4 -6.5 -3.0 0.0 0.0 2.0 0.2 0.0 0.0 0.0 0.0 ! bottom gearbox and crankset 5 -13.2 -3.0 0.0 -5.0 3.0 0.2 0.0 0.0 0.0 0.0 End #====================== Engine # KPeng IEtyp Nbeam t Xp Yp Zp Tx Ty Tz dFdPe dMdPe Rdisk Omega CdA 1 0 4 -6.5 -6.5 0. 0. -1.0 0.0 0.0 1. 0. 5.5 12.5 0.0125 End #============ Beam 1 Wing # t chord y Ccg * 1.0 1.0 1.0 1.0 00.00 3.75 00.00 0.1875 14.00 3.75 14.00 0.1875 14.00 3.75 14.00 0.1875 42.00 2.50 42.00 0.125 42.00 2.50 42.00 0.125 55.42 1.25 55.42 0.0625 55.42 1.25 55.42 0.0625 56.00 0.625 56.00 0.03125 # t z 0.0 0.5 56.0 0.5 # t Cshell Nshell Atshell * 1.0 0.04167 0.04167 0.00058 00.00 3.50 3.50 0.70 14.00 3.50 3.50 0.40 14.00 3.25 3.25 0.40 24.00 3.25 3.25 0.30 24.00 3.25 3.25 0.30 32.00 2.25 2.25 0.15 32.00 2.25 2.25 0.15 42.00 2.25 2.25 0.08 42.00 1.75 1.75 0.08 50.00 1.75 1.75 0.05 50.00 1.25 1.25 0.05 56.00 1.25 1.25 0.03 # t alpha Cm Cdf Cdp * 1.0 1.0 1.0 1.0 1.0 00.00 1.40 -0.135 0.0060 0.005 28.00 1.40 -0.135 0.0060 0.005 28.00 1.40 -0.135 0.0060 0.005 42.00 1.40 -0.140 0.0070 0.005 42.00 1.40 -0.140 0.0070 0.005 45.50 1.20 -0.140 0.0072 0.005 49.00 0.85 -0.140 0.0077 0.005 51.33 0.15 -0.140 0.0085 0.005 53.00 -0.85 -0.155 0.0090 0.005 54.667 -3.05 -0.140 0.0082 0.005 55.42 -4.85 -0.070 0.0075 0.005 56.00 -6.85 -0.050 0.0070 0.005 # t dCLda * 1.0 1.0 0.0 6.35 56.0 6.35 # t CLmax CLmin * 1.0 1.0 1.0 0.0 1.7 -0.8 56.0 1.7 -0.8 # ! t dCLdF3 dCMdF3 !* 1.0 0.01745 0.01745 ! 0.0 6.2 -0.9 ! 56.0 6.2 -0.9 # t twist * 1.0 1.0 0.0 8.2 56.0 8.2 # t Xax * 1.0 1.0 0.0 0.33 56.0 0.33 # t EIcc EInn * 1.0 1.00E4 1.0E6 0.0 5.03 1.65 2.0 5.03 1.65 4.0 5.03 1.65 6.0 5.21 1.66 8.0 5.27 1.65 10.0 5.61 1.66 12.0 5.78 1.66 14.0 5.78 1.59 16.0 6.38 1.29 18.0 7.02 1.20 20.0 7.60 1.13 22.0 8.11 1.08 24.0 8.39 1.01 26.0 9.00 0.962 28.0 9.55 0.901 28.0 9.55 0.901 30.0 6.89 0.854 32.0 5.08 0.775 34.0 3.73 0.712 36.0 2.40 0.452 38.0 2.16 0.395 40.0 1.84 0.360 42.0 1.35 0.326 44.0 0.829 0.179 46.0 0.614 0.139 48.0 0.379 0.104 50.0 0.160 0.080 52.0 0.120 0.060 54.0 0.080 0.040 56.0 0.040 0.020 # t GJ * 1.0 1.0E4 0.0 4.08 1.0 4.08 2.0 4.08 3.0 4.08 5.0 4.08 6.0 4.08 7.0 4.08 7.0 3.42 8.0 3.42 9.0 3.42 10.0 3.42 11.0 3.44 12.0 3.44 13.0 3.44 14.0 3.44 14.0 2.27 15.0 2.27 16.0 2.29 17.0 2.30 18.0 2.31 19.0 2.32 20.0 2.33 21.0 2.33 22.0 2.34 23.0 2.35 24.0 2.35 25.0 2.36 26.0 2.37 27.0 2.38 28.0 2.39 28.0 2.30 30.0 1.80 31.0 1.60 32.0 1.57 33.0 1.40 34.0 1.13 35.0 0.875 36.0 0.674 37.0 0.668 38.0 0.668 39.0 0.665 40.0 0.658 41.0 0.645 42.0 0.638 42.0 0.320 44.0 0.313 45.0 0.311 46.0 0.305 47.0 0.301 48.0 0.240 49.0 0.113 49.0 0.0735 51.0 0.0735 52.0 0.0735 53.0 0.0735 54.0 0.0735 55.0 0.0735 56.0 0.0735 # t mg * 1.0 1.0 0.0 0.610 2.0 0.495 4.0 0.465 6.0 0.462 8.0 0.445 10.0 0.432 12.0 0.434 16.0 0.424 18.0 0.428 20.0 0.432 22.0 0.438 24.0 0.438 26.0 0.444 28.0 0.435 30.0 0.408 31.0 0.361 32.0 0.350 33.0 0.329 34.0 0.317 35.0 0.305 36.0 0.294 38.0 0.285 40.0 0.273 42.0 0.215 44.0 0.165 46.0 0.152 48.0 0.138 50.0 0.105 52.0 0.099 54.0 0.094 56.0 0.090 End #============ Beam 2 Stab # t chord x y z Ccg * 1. 1. 1. 1. 1. 1. 0.0 1.85 17.5 0.0 1.0 0.09 7.5 1.05 17.5 7.5 1.0 0.05 # t Cshell Nshell Atshell * 1.0 0.007 0.007 0.000050 0.0 0.50 0.50 0.025 3.0 0.50 0.50 0.015 3.0 0.375 0.375 0.015 7.5 0.375 0.375 0.010 # t alpha Cm Cdf * 1.0 1.0 1.0 1.0 0.0 2.0 0.0 0.015 7.5 2.0 0.0 0.015 # t dCLda * 1.0 1.0 0.0 6.2 7.5 6.2 # t dCLdF2 * 1.0 0.01745 0.0 6.2 7.5 6.2 # t CLmax CLmin * 1.0 1.0 1.0 0.0 1.1 -1.1 7.5 1.1 -1.1 # t twist * 1.0 1.0 0.0 0.0 7.5 0.0 # t Xax * 1.0 1.0 0.0 0.25 7.5 0.25 # t EIcc EInn GJ * 1.0 3.0 5.0E3 2.0 0.0 180.0 1.0 40.0 2.0 120.0 0.7 36.0 4.0 70.0 0.38 30.0 7.0 30.0 0.11 14.0 7.5 25.0 0.1 11.0 # t mg * 1.0 0.10 0.0 0.95 1.0 0.95 1.0 0.95 7.5 0.50 End #============ Beam 3 Rudder # t chord x y z Ccg * 1. 1. 1. 1. 1. 1. -3.5 2.2 20.0 1.0 -3.5 0.11 0.0 3.5 20.0 1.0 0.0 0.175 0.0 3.5 20.0 1.0 0.0 0.175 5.0 1.5 20.0 1.0 5.0 0.075 # t Cshell Nshell Atshell * 1.0 0.007 0.007 0.000050 -3.5 0.50 0.50 0.025 2.0 0.50 0.50 0.025 2.0 0.375 0.375 0.015 5.0 0.375 0.375 0.010 # t alpha Cm Cdf * 1.0 1.0 1.0 1.0 -3.5 0.0 0.0 0.015 5.0 0.0 0.0 0.015 # t dCLda * 1.0 1.0 -3.5 6.2 5.0 6.2 # t dCLdF3 * 1.0 -0.01745 -3.5 6.2 5.0 6.2 !# t CLmax CLmin * 1.0 1.0 1.0 -3.5 1.1 -1.1 5.0 1.1 -1.1 # t Xax * 1. 1. -3.5 0.25 5.0 0.25 # t EIcc EInn GJ * 1.0 2.5 5.0E3 4.0 -3.5 30.0 0.5 15.0 -2.0 60.0 0.75 17.5 0.0 200.0 1.0 20.0 0.0 200.0 1.0 20.0 2.0 85.0 0.5 15.0 4.0 35.0 0.25 7.0 5.0 27.0 0.20 5.5 # t mg * 1.0 0.18 -3.5 0.40 0.0 0.95 0.0 0.95 1.0 0.95 1.0 0.95 5.0 0.55 End #============ Beam 4 Tailboom # t x y z * 1.0 1.0 1.0 1.0 -6.5 -6.5 0.0 0.0 20.0 20.0 0.0 0.0 # t Cshell Nshell Atshell radius * 1.0 0.04167 0.04167 0.00058 0.04167 -6.50 3.25 3.25 0.40 3.25 4.00 3.25 3.25 0.40 3.25 4.00 3.25 3.25 0.40 3.25 12.00 2.25 2.25 0.20 2.25 12.00 2.25 2.25 0.20 2.25 20.00 2.25 2.25 0.20 2.25 # t EIcc EInn GJ * 1.0 0.50E4 0.50E4 0.50E4 -6.5 10.00 10.00 5.00 4.0 20.00 20.00 5.00 4.0 20.00 20.00 5.00 12.0 2.20 2.20 2.20 12.0 2.20 2.20 2.20 20.0 1.50 1.50 1.50 # t mg * 1.0 1.0 -6.5 0.150 4.0 0.150 4.0 0.150 12.0 0.110 12.0 0.110 20.0 0.060 End #============ Beam 5 Fairing # t x y z chord Xax * 1.0 1.0 1.0 1.0 1. 1. -15.6 2.5 0.0 -5.6 6.0 1.2 -15.2 2.5 0.0 -5.2 8.5 0.95 -15.2 2.5 0.0 -5.2 8.5 0.95 -14.7 2.5 0.0 -4.7 9.0 0.89 -13.2 2.5 0.0 -3.2 8.0 0.72 -13.2 2.5 0.0 -3.2 8.0 0.72 -12.4 2.5 0.0 -2.4 6.6 0.655 -11.6 2.5 0.0 -1.6 5.2 0.554 -10.8 2.5 0.0 -0.8 3.8 0.379 -10.4 2.5 0.0 -0.4 3.1 0.232 -10.0 2.5 0.0 0.0 2.4 0.0 # t alpha Cm Cdf Cdp * 1.0 1.0 1.0 1.0 1.0 -15.6 0.0 0.0 0.015 0.010 -10.0 0.0 0.0 0.015 0.010 # t dCLda * 1.0 1.0 -15.6 6.2 -10.0 6.2 # t CLmax CLmin * 1.0 1.0 1.0 -15.6 1.1 -1.1 -10.0 1.1 -1.1 # t EIcc EInn GJ * 1.0 4.00E4 8.00E4 4.00E4 -15.6 5.00 5.00 5.00 -10.0 5.00 5.00 5.00 # t mg * 1.0 1.0 -15.6 0.750 -13.2 0.750 -13.2 0.750 -10.0 0.750 End