87 lines
2.7 KiB
Text
87 lines
2.7 KiB
Text
# Jeff Scott
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# DHC-6 Twin Otter
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# small twin turboprop engine commuter aircraft
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# This model was developed by Devesh Pokhariyal of the Smart Icing
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# Systems Aerodynamics group (Prof. Michael Bragg, head) at the
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# University of Illinois. The aircraft data is from:
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# Pokhariyal, Devesh and Merret, Jason. FDC flight simulator
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# Twin Otter input file (version5_bat), 5/23/00.
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# 05-23-2000 file creation
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geometry bw 65.0 # [ft]
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geometry cbar 6.5 # [ft]
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geometry Sw 420.0 # [ft^2]
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controlSurface de 20 20 # [deg] guess for now
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controlSurface da 20 20 # [deg] guess for now
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controlSurface dr 20 20 # [deg] guess for now
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#controlSurface set_Long_trim_deg -3.0
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#controlSurface elevator_input Aircraft-uiuc/TwinOtter/deft.dat 1 0 700
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mass Weight 10141 # [lb]
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mass I_xx 16039.3 # [slug-ft^2]
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mass I_yy 22841.6 # [slug-ft^2]
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mass I_zz 35807.4 # [slug-ft^2]
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mass I_xz 1102.8 # [slug-ft^2]
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# aircraft specs: 2 engines of 462 kW each
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# ~2000 lb static thrust each
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engine simpleSingle 2000 # [lb]
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CL CZo -0.360 # []
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CL CZ_a -5.660 # [/rad]
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#CL CZ_a2 0.0 # [/rad]
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#CL CZ_a3 0.0 # [/rad]
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CL CZ_q -19.97 # [/rad]
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CL CZ_de -0.608 # [/rad]
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#CL CZ_deb2 0.0 # [/rad]
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#CL CZ_df 0.0 # [/rad]
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#CL CZ_adf 0.0 # [/rad]
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CD CXo -0.0488 # []
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CD CX_a 0.223 # [/rad]
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CD CX_a2 1.659 # [/rad]
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#CD CX_a3 0.0 # [/rad]
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#CD CX_q 0.0 # [/rad]
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#CD CX_de 0.0 # [/rad]
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#CD CX_dr 0.0 # [/rad]
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#CD CX_df 0.0 # [/rad]
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#CD CX_adf 0.0 # [/rad]
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Cm Cmo 0.040 # []
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Cm Cm_a -1.310 # [/rad]
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#Cm Cm_a2 0.0 # [/rad]
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Cm Cm_q -34.2 # [/rad]
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Cm Cm_de -1.740 # [/rad]
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#Cm Cm_b2 0.0 # [/rad]
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#Cm Cm_r 0.0 # [/rad]
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#Cm Cm_df 0.0 # [/rad]
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#CY CYo 0.0 # []
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CY CY_beta -0.6 # [/rad]
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CY CY_p -0.2 # [/rad]
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CY CY_r 0.4 # [/rad]
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#CY CY_da 0.0 # [/rad]
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CY CY_dr 0.15 # [/rad]
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#CY CY_dra 0.0 # [/rad]
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#CY CY_bdot 0.0 # [/rad]
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#Cl Clo 0.0 # []
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Cl Cl_beta -0.08 # [/rad]
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Cl Cl_p -0.5 # [/rad]
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Cl Cl_r 0.06 # [/rad]
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Cl Cl_da -0.15 # [/rad]
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Cl Cl_dr 0.015 # [/rad]
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#Cl Cl_daa 0.0 # [/rad]
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#Cn Cno 0.0 # [/rad]
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Cn Cn_beta 0.1 # [/rad]
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Cn Cn_p -0.06 # [/rad]
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Cn Cn_r -0.18 # [/rad]
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Cn Cn_da -0.001 # [/rad]
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Cn Cn_dr -0.125 # [/rad]
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#Cn Cn_q 0.0 # [/rad]
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#Cn Cn_b3 0.0 # [/rad]
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