#************************************
#Sample "HERSEY BAR" wing AVL dataset
#Design variables specified
#************************************
SWEPT HERSEY BAR Wing with Design Variables
#Mach
 0.0    
#IYsym   IZsym   Zsym
 1       0       0.0
#Sref    Cref    Bref
3.894    0.708   5.5
#Xref    Yref    Zref
0.177    0.0     0.0
#
SURFACE 
WING 
#Nchordwise  Space
 8           1.0
#
SECTION
#Xle    Yle    Zle     Chord   Ainc  Nspanwise  Space
0.000   0.000  0.000   0.708    0.     7         2.0
DESIGN
Des1 1.0
#
SECTION
#Xle    Yle    Zle     Chord   Ainc  Nspanwise  Space
0.500   1.375  0.000   0.708    0.     3        -2.8
DESIGN
Des2 1.0
#
SECTION
#Xle    Yle    Zle     Chord   Ainc  Nspanwise  Space
0.800   2.20   0.000   0.708    0.     3        -2.5
DESIGN
Des3 1.0
#
SECTION
#Xle    Yle    Zle     Chord   Ainc  Nspanwise  Space
0.950   2.6125 0.000   0.708    0.     3        -2.0
DESIGN
Des4 1.0
#
SECTION
#Xle    Yle    Zle     Chord   Ainc  Nspanwise  Space
1.000   2.75   0.000   0.708    0.     0         0.0
DESIGN
Des5 1.0