Square wing
0.0                   !   Mach
0     0     0.0       !   iYsym  iZsym  Zsym
 1.0  1.0   1.0       !   Sref   Cref   Bref   reference area, chord, span
 0.25 0.0   0.0       !   Xref   Yref   Zref   moment reference location (arb.)
0.0                   !   CDp
#
#==============================================================
#
SURFACE
Wing
24  1.0    24  -2.0  ! Nchord   Cspace   Nspan  Sspace
#
YDUPLICATE
0.0
#
# twist angle bias for whole surface
ANGLE
     0.00000    
#
SCALE
  1.0   1.0   0.0
#
# x,y,z bias for whole surface
TRANSLATE
    0.  0.  0. 
#
#-----------------------------
SECTION
     0.0          0.0        0.0         1.0         0.000 
#-----------------------------
SECTION
    0.0           0.5        0.0         1.0         0.000  
#-----------------------------