65 lines
1.8 KiB
Text
65 lines
1.8 KiB
Text
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# Jeff Scott
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# Cessna 310, cruise configuration
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# small twin piston engine general aviation airplane, data from:
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# Roskam, Jan. Airplane Flight Dynamics and Automatic Flight
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# Controls, Part I. Lawrence KS: DARcorporation, 1995,
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# pg 487-489
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# 03-23-2000 file creation
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init Dz_cg 2.5 # [ft]
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geometry bw 36.9 # [ft]
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geometry cbar 4.79 # [ft]
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geometry Sw 175.0 # [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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mass Weight 4600 # [lb]
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mass I_xx 8884 # [slug-ft^2]
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mass I_yy 1939 # [slug-ft^2]
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mass I_zz 11001 # [slug-ft^2]
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mass I_xz 0 # [slug-ft^2]
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# Roskam: CTx=0.031 (cruise conditions) --> 500 lb
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# aircraft specs: 2 engines of 213 kW each
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# ~1100 lb static thrust each
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engine simpleSingle 1100 # [lb]
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CL CLo 0.288 # []
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CL CL_a 4.58 # [/rad]
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CL CL_adot 5.3 # [/rad]
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CL CL_q 9.7 # [/rad]
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CL CL_de 0.81 # [/rad]
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CD CDo 0.029 # []
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CD CD_a 0.16 # [/rad]
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CD CD_de 0.0 # [/rad]
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Cm Cmo 0.07 # []
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Cm Cm_a -0.137 # [/rad]
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Cm Cm_adot -12.7 # [/rad]
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Cm Cm_q -26.3 # [/rad]
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Cm Cm_de -2.26 # [/rad]
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CY CY_beta -0.698 # [/rad]
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CY CY_p -0.141 # [/rad]
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CY CY_r 0.355 # [/rad]
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CY CY_da 0.0 # [/rad] sign reversed
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CY CY_dr 0.23 # [/rad]
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Cl Cl_beta -0.1096 # [/rad]
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Cl Cl_p -0.551 # [/rad]
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Cl Cl_r 0.0729 # [/rad]
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Cl Cl_da -0.172 # [/rad] sign reversed
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Cl Cl_dr 0.0192 # [/rad]
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Cn Cn_beta 0.1444 # [/rad]
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Cn Cn_p -0.0257 # [/rad]
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Cn Cn_r -0.1495 # [/rad]
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Cn Cn_da 0.0168 # [/rad] sign reversed
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Cn Cn_dr -0.1152 # [/rad]
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