!***************************************
!Sample AVL input dataset
!***************************************
Sample Airplane
!Mach
 0.0    
!IYsym   IZsym   Zsym
 0       0       0.0
!Sref    Cref    Bref
7.80     0.78    10.0
!Xref    Yref    Zref
0.5      0.0      0.0
!
SURFACE 
WING 
!Nchordwise  Cspace
6            1.0
YDUPLICATE 
0.0
SECTION
!Xle    Yle    Zle     Chord   Ainc  Nspanwise  Sspace
0.      0.     0.      1.000   0.    8          1.0
SECTION
!Xle    Yle    Zle     Chord   Ainc  Nspanwise  Sspace
0.2     3.0    0.2     0.800   0.    7          1.0
SECTION
!Xle    Yle    Zle     Chord   Ainc  Nspanwise  Sspace
0.6     5.0    0.5     0.400   0.    0          0
!
SURFACE
STAB
!Nchordwise  Space
5            1.0
YDUPLICATE 
0.0
SECTION
!Xle    Yle    Zle     Chord   Ainc  Nspanwise  Sspace
2.0     0.     -0.2    0.8     0.    7          -1.25
SECTION
!Xle    Yle    Zle     Chord   Ainc  Nspanwise  Sspace
2.8     1.80   -0.6    0.3     0.    0          0
SURFACE
FIN
!Nchordwise  Space
5            1.0
SECTION
!Xle    Yle    Zle     Chord   Ainc  Nspanwise  Sspace
1.80    0.     -0.2    0.8     0.    7          -1.25
SECTION
!Xle    Yle    Zle     Chord   Ainc  Nspanwise  Sspace
2.6     0.     1.0     0.3     0.    0          0
END