#***************************************
#AVL dataset for Aerosond wing/tail
#***************************************
AEROSONDE
#Mach
 0.0    
#IYsym   IZsym   Zsym
 0       0       0.0
#Sref    Cref    Bref
0.6204   0.2113  2.938
#Xref    Yref    Zref
0.07     0.0      0.0
#
#===================================
SURFACE 
Wing
#Nchordwise  Ccpace  Nspanwise  Sspace
8            1.0     14         -2.0
YDUPLICATE
0.0

SECTION
#Xle    Yle    Zle     Chord   Ainc
0.      0.     0.      0.254    3.  
AFILE
sd7037.dat

SECTION
#Xle    Yle    Zle     Chord   Ainc
0.0172  0.6226 0.      0.2287   3. 
CONTROL
aileron  -1.0  0.77  0. 0. 0.  -1.
AFILE
sd7037.dat

SECTION
#Xle    Yle    Zle     Chord   Ainc
0.0407  1.469  0.1193  0.150    3.  
CONTROL
aileron  -1.0  0.77  0. 0. 0.  -1.
AFILE
sd7037.dat

#
#===================================
SURFACE 
Tail
#Nchordwise  Cspace   Nspanwise   Sspace
8            1.0       8          1.0
YDUPLICATE
0.0

SECTION
#Xle    Yle    Zle     Chord   Ainc  
1.069   0.     0.45    0.1143   0.  
CONTROL
elevator  1.0  0.70  0. 0. 0.   1.
CONTROL
rudder   -1.0  0.70  0. 0. 0.  -1.

SECTION
#Xle    Yle    Zle     Chord   Ainc
1.069   0.45   0.10      0.1143   0. 
CONTROL
elevator  1.0  0.70  0. 0. 0.   1.
CONTROL
rudder   -1.0  0.70  0. 0. 0.  -1.