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fgdata/Aircraft-uiuc/TwinOtterAllIce/aircraft.dat
2000-10-22 21:05:31 +00:00

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4.8 KiB
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# Jeff Scott
# DHC-6 Twin Otter
# small twin turboprop engine commuter aircraft with simulated
# icing characteristics (entire aircraft iced)
# This model was developed by Devesh Pokhariyal of the Smart Icing
# Systems Aerodynamics group (Prof. Michael Bragg, head) at the
# University of Illinois. The aircraft data is from:
# Pokhariyal, Devesh and Merret, Jason. FDC flight simulator
# Twin Otter input file (version5_bat), 5/23/00.
# Pokhariyal, Devesh and Merret, Jason. FDC flight simulator
# Twin Otter icing file (icesev_bat), 5/30/00.
# Ratvasky, T.P. and Ranaudo, R.J. "Icing Effects on Aircraft
# Stability and Control Determined from Flight Data," 31st
# Aerospace Sciences Meeting and Exhibit, 11-14 Jan 1993,
# AIAA-93-0398.
# 05-30-2000 file creation
geometry bw 65.0 # [ft]
geometry cbar 6.5 # [ft]
geometry Sw 420.0 # [ft^2]
geometry bh 20.7 # [ft] AIAA 93-0398 Table 1
geometry ch 4.8 # [ft] AIAA 93-0398 Table 1
geometry Sh 97.8 # [ft^2] AIAA 93-0398 Table 1
controlSurface de 20 20 # [deg] guess for now
controlSurface da 20 20 # [deg] guess for now
controlSurface dr 20 20 # [deg] guess for now
mass Weight 10141 # [lb]
mass I_xx 16039.3 # [slug-ft^2]
mass I_yy 22841.6 # [slug-ft^2]
mass I_zz 35807.4 # [slug-ft^2]
mass I_xz 1102.8 # [slug-ft^2]
# aircraft specs: 2 engines of 462 kW each
# ~2000 lb static thrust each
engine simpleSingle 2000 # [lb]
CL CZo -0.360 # []
CL CZ_a -5.660 # [/rad]
#CL CZ_a2 0.0 # [/rad]
#CL CZ_a3 0.0 # [/rad]
CL CZ_q -19.97 # [/rad]
CL CZ_de -0.608 # [/rad]
#CL CZ_deb2 0.0 # [/rad]
#CL CZ_df 0.0 # [/rad]
#CL CZ_adf 0.0 # [/rad]
CD CXo -0.0488 # []
CD CX_a 0.223 # [/rad]
CD CX_a2 1.659 # [/rad]
#CD CX_a3 0.0 # [/rad]
#CD CX_q 0.0 # [/rad]
#CD CX_de 0.0 # [/rad]
#CD CX_dr 0.0 # [/rad]
#CD CX_df 0.0 # [/rad]
#CD CX_adf 0.0 # [/rad]
Cm Cmo 0.040 # []
Cm Cm_a -1.310 # [/rad]
#Cm Cm_a2 0.0 # [/rad]
Cm Cm_q -34.2 # [/rad]
Cm Cm_de -1.740 # [/rad]
#Cm Cm_b2 0.0 # [/rad]
#Cm Cm_r 0.0 # [/rad]
#Cm Cm_df 0.0 # [/rad]
#CY CYo 0.0 # []
CY CY_beta -0.6 # [/rad]
CY CY_p -0.2 # [/rad]
CY CY_r 0.4 # [/rad]
#CY CY_da 0.0 # [/rad]
CY CY_dr 0.15 # [/rad]
#CY CY_dra 0.0 # [/rad]
#CY CY_bdot 0.0 # [/rad]
#Cl Clo 0.0 # []
Cl Cl_beta -0.08 # [/rad]
Cl Cl_p -0.5 # [/rad]
Cl Cl_r 0.06 # [/rad]
Cl Cl_da -0.15 # [/rad]
Cl Cl_dr 0.015 # [/rad]
#Cl Cl_daa 0.0 # [/rad]
#Cn Cno 0.0 # [/rad]
Cn Cn_beta 0.1 # [/rad]
Cn Cn_p -0.06 # [/rad]
Cn Cn_r -0.18 # [/rad]
Cn Cn_da -0.001 # [/rad]
Cn Cn_dr -0.125 # [/rad]
#Cn Cn_q 0.0 # [/rad]
#Cn Cn_b3 0.0 # [/rad]
ice iceTime 120 # [s]
ice transientTime 30 # [s]
ice eta_ice_final 0.3 # [] do not set higher than about 0.4!
ice kCXo 6.52696 # []
ice kCX_a -0.14296 # []
ice kCX_a2 -1.59837 # []
#ice kCX_a3 0.0 # []
#ice kCX_q 0.0 # []
#ice kCX_de 0.0 # []
#ice kCX_df 0.0 # []
#ice kCX_dr 0.0 # []
#ice kCX_adf 0.0 # []
ice kCZo 0.0 # []
ice kCZ_a -1.48148 # []
#ice kCZ_a2 0.0 # []
#ice kCZ_a3 0.0 # []
ice kCZ_q -0.20741 # []
ice kCZ_de -1.40741 # []
#ice kCZ_df 0.0 # []
#ice kCZ_adf 0.0 # []
#ice kCZ_deb2 0.0 # []
ice kCmo 0.0 # []
ice kCm_a -1.46667 # []
#ice kCm_a2 0.0 # []
#ice kCm_b2 0.0 # []
ice kCm_q -0.51852 # []
#ice kCm_r 0.0 # []
ice kCm_de -1.48148 # []
#ice kCm_df 0.0 # []
#ice kCYo 0.0 # []
ice kCY_beta -2.96296 # []
ice kCY_p 0.0 # []
ice kCY_r 0.0 # []
#ice kCY_da 0.0 # []
ice kCY_dr -1.18519 # []
#ice kCY_dra 0.0 # []
#ice kCY_bdot 0.0 # []
#ice kClo 0.0 # []
ice kCl_beta -1.48148 # []
ice kCl_p -1.48148 # []
ice kCl_r 0.0 # []
ice kCl_da -1.48148 # []
ice kCl_dr -1.18519 # []
#ice kCl_daa 0.0 # []
#ice kCno 0.0 # []
ice kCn_beta -2.96296 # []
#ice kCn_b3 0.0 # []
ice kCn_p 0.0 # []
#ice kCn_q 0.0 # []
ice kCn_r -0.88889 # []
ice kCn_da 0.0 # []
ice kCn_dr -1.18519 # []
ice beta_probe_wing 5.0 # [ft]
ice beta_probe_tail 3.5 # [ft]