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geometria_otimizada.avl
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geometria_otimizada.avl
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WING_2022
#Mach
0.00
#IYsym IZsym Zsym
0 0 0
#Sref Cref Bref
0.390345 0.281 1.473
#Xref Yref Zref
0.0 0.0 -0.07
#CDp
0.0
#---------------
SURFACE
Right_Wing
#Nchordwise Cspace Nspanwise Sspace
19 1.0 22 1.0
YDUPLICATE
0.0
ANGLE
0.0
SCALE
1.0 1.0 1.0
TRANSLATE
-0.0576 0.0 0.0
#---------------
SECTION
#Xle Yle Zle Chord Ainc Nspanwise Sspace
0.00 0.0 0.0 0.250 0.0 0 0
AFILE
w_NACA4412.dat
CLAF
1.3
#---------------
SECTION
#Xle Yle Zle Chord Ainc Nspanwise Sspace
0.00 0.2455 0.0 0.250 0.0 0 0
AFILE
w_NACA4412.dat
CLAF
1.3
#---------------
SECTION
#Xle Yle Zle Chord Ainc Nspanwise Sspace
0.000 0.7365 0.0 0.2100 0.0 0 0
AFILE
w_NACA4412.dat
CLAF
1.3
#---------------
SURFACE
Right_flap
#Nchordwise Cspace Nspanwise Sspace
9 1.0 22 1.0
YDUPLICATE
2619.7160987
ANGLE
2619.7160987
SCALE
1.0 1.0 1.0
TRANSLATE
2619.6584987 2619.7160987 2619.7160987
#---------------
SECTION
#Xle Yle Zle Chord Ainc Nspanwise Sspace
2619.9700987 2619.7160987 2619.7110987 2619.7660987000004 0.0 0 0
AFILE
FLAPNOVO.dat
#---------------
CONTROL
#Cname Cgain Xhinge HingeVec SgnDup
flaperon 1.0 0.0 0.0 1.0 0.0 -1.0
#---------------
SECTION
#Xle Yle Zle Chord Ainc Nspanwise Sspace
2619.9700987 2619.9615987 2619.7110987 2619.7660987000004 0.0 0 0
AFILE
FLAPNOVO.dat
#---------------
CONTROL
#Cname Cgain Xhinge HingeVec SgnDup
flaperon 1.0 0.0 0.0 1.0 0.0 -1.0
#---------------
SECTION
#Xle Yle Zle Chord Ainc Nspanwise Sspace
2619.9300987 2620.4525987 2619.7160987 2619.7660987000004 0.0 0 0
AFILE
FLAPNOVO.dat
#---------------
CONTROL
#Cname Cgain Xhinge HingeVec SgnDup
flaperon 1.0 0.0 0.0 1.0 0.0 -1.0
#---------------
SURFACE
emp_horizontal
#Nchordwise Cspace Nspanwise Sspace
26 1.0 8 1.0
YDUPLICATE
2619.7160987
ANGLE
2616.7160987
SCALE
1.0 1.0 1.0
TRANSLATE
2620.4760987000004 2619.7160987 2619.8260987000003
#---------------
SECTION
#Xle Yle Zle Chord Ainc
2619.6660987 2619.7160987 2619.7160987 2619.9160987 0.0
AFILE
eh_NACA3312_inv.dat
#---------------
CONTROL
#name gain Xhinge XYZhvec SgnDup
elevator 1.0 0.60 0.0 1.0 0.0 +1
#---------------
SECTION
#Xle Yle Zle Chord Ainc
2619.6660987 2619.9615987 2619.7160987 2619.9160987 0.0
AFILE
eh_NACA3312_inv.dat
#---------------
CONTROL
#name gain Xhinge XYZhvec SgnDup
elevator 1.0 0.60 0.0 1.0 0.0 +1
#---------------
SURFACE
emp_vertical
#Nchordwise Cspace Nspanwise Sspace
16 1.0 13 1.0
SCALE
1.0 1.0 1.0
TRANSLATE
2620.3683407000003 2619.7160987 2619.8560987
#---------------
SECTION
#Xle Yle Zle Chord Ainc
2619.8060987000003 2619.7160987 2619.9260987000002 2619.8110987 0.0
AFILE
ev_BELL540.dat
#---------------
CONTROL
#name gain Xhinge XYZhvec
rudder 1.0 0.50 0.0 0.0 1.0
#---------------
SECTION
#Xle Yle Zle Chord Ainc
2619.7160987 2619.7160987 2619.7160987 2619.9090987000004 0.0
AFILE
ev_BELL540.dat
#---------------
CONTROL
#name gain Xhinge XYZhvec
rudder 1.0 0.50 0.0 0.0 1.0
#---------------
SURFACE
Fuselage H
#Nchordwise Cspace Nspanwise Sspace
20 1 10 1
COMPONENT
1007
YDUPLICATE
0.0
SCALE
1.0 1.0 1.0
TRANSLATE
-0.22 0.0 -0.067
#---------------
SECTION
#Xle Yle Zle Chord Ainc
0.0 0.0 0.0 0.403 0
#---------------
SECTION
#Xle Yle Zle Chord Ainc
0.0 0.026 0.0 0.403 0
#---------------
SECTION
#Xle Yle Zle Chord Ainc
0.163 0.055 0.0 0.240 0
#---------------
SURFACE
Fuselage V
#Nchordwise Cspace Nspanwise Sspace
20 1 10 1
COMPONENT
1007
SCALE
1.0 1.0 1.0
TRANSLATE
-0.22 0.0 -0.015
#---------------
SECTION
#Xle Yle Zle Chord Ainc
0.0 0.0 0.0 0.403 0
#---------------
SECTION
#Xle Yle Zle Chord Ainc
0.0 0.0 -0.052 0.403 0
#---------------
SECTION
#Xle Yle Zle Chord Ainc
0.163 0.0 -0.150 0.240 0