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in_improved_1.avl
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in_improved_1.avl
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WING_2022
#Mach
0.00
#IYsym IZsym Zsym
0 0 0
#Sref Cref Bref
0.39 0.232 1.67
#Xref Yref Zref
0.0 0.0 0.0
#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
-0.058 0.0 0.0
#---------------
SECTION
#Xle Yle Zle Chord Ainc Nspanwise Sspace
0.00 0.0 0.0 0.232 0.0 0 0
AFILE
MMT19012-10.dat
CLAF
1.3
#---------------
SECTION
#Xle Yle Zle Chord Ainc Nspanwise Sspace
0.000 0.835 0.0 0.232 0.0 0 0
AFILE
MMT19012-10.dat
CLAF
1.3
#---------------
CONTROL
#Cname Cgain Xhinge HingeVec SgnDup
aileron 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
0.0
ANGLE
-3.0
SCALE
1.0 1.0 1.0
TRANSLATE
0.76 0.0 0.11
#---------------
SECTION
#Xle Yle Zle Chord Ainc
<<<<<<< HEAD:env/in_0.avl
<__main__.Input object at 0x7fb8180e79d0> 0.0 <__main__.Input object at 0x7fb8180e7a30> <__main__.Input object at 0x7fb8180e7a90> <__main__.Input object at 0x7fb8180e7af0>
=======
-1.155000000000001 0.0 -0.09000000000000001 -0.0200000000000001 0.0
Ainc
0.0
>>>>>>> 4a33cf4db4320e36410c9e990fd9e1d8764ca19a:in_improved_1.avl
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
<__main__.Input object at 0x7fb8180e7b50> <__main__.Input object at 0x7fb8180e7bb0> 0 <__main__.Input object at 0x7fb8180e7c10> <__main__.Input object at 0x7fb8180e7c70>
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
0.652242 0.0 0.14
#---------------
SECTION
#Xle Yle Zle Chord Ainc
<__main__.Input object at 0x7fb8180e7b50> 0 <__main__.Input object at 0x7fb8180e7a90> <__main__.Input object at 0x7fb8180e79d0> 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
<__main__.Input object at 0x7fb8180e7970> 0 <__main__.Input object at 0x7fb8180e7ee0> <__main__.Input object at 0x7fb8180e7d00> 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 0.485 0
#---------------
SECTION
#Xle Yle Zle Chord Ainc
0.0 0.031 0.0 0.485 0
#---------------
SECTION
#Xle Yle Zle Chord Ainc
0.205 0.059 0.0 0.280 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 0.485 0
#---------------
SECTION
#Xle Yle Zle Chord Ainc
0.0 0.0 -0.062 0.485 0
#---------------
SECTION
#Xle Yle Zle Chord Ainc
0.205 0.0 -0.205 0.280 0