Allegro-lite 2M
0.0                      Mach
0     0     0.0          iYsym  iZsym  Zsym
530.0 6.6  78.6          Sref   Cref   Bref   reference area, chord, span
3.250 0.0   0.5          Xref   Yref   Zref   moment reference location (arb.)
0.020                    CDoref
#
#==============================================================
#
SURFACE
WING
7  1.0  20  -2.0  !  Nchord   Cspace   Nspan  Sspace
#
# reflect image wing about y=0 plane
YDUPLICATE
     0.00000 
#
# twist angle bias for whole surface
ANGLE
     0.00000    
#
# x,y,z bias for whole surface
TRANSLATE
    0.00000     0.00000     0.00000
#--------------------------------------------------------------
#    Xle         Yle         Zle         chord       angle   Nspan  Sspace
SECTION
     0.00000     0.00000     0.00000     8.0         1.490   5      0.25
AFIL
ag35.dat
#-----------------------
SECTION
     0.500       15.0        0.0         7.5         1.380   7     -2.60
AFIL
ag36.dat
#-----------------------
SECTION
     1.875       31.0        3.30        6.0         1.220   8     -2.25
AFIL
ag37.dat
#-----------------------
SECTION
     3.625       39.3        7.00        4.0         0.940   1      0
AFIL
"ag38.dat" 0 1
#
#==============================================================
#
SURFACE
Horizontal tail
5  1.0  7  -1.5  ! Nchord   Cspace
#
YDUPLICATE
     0.00000
ANGLE
     0.0000
TRANSLATE
    27.50000     0.00000     1.25000
#--------------------------------------------------------------
SECTION
     0.00000     0.00000     0.00000     3.5         0.000   7  -1.5

CONTROL
elevator  1.0  0.0  0.0 1.0 0.0  1.0
#-----------------------
SECTION
     1.15        9.0         0.00000     1.8         0.000   1   0

CONTROL
elevator  1.0  0.0  0.0 1.0 0.0  1.0
#
#==============================================================
#
SURFACE
Vertical tail
6  1.0  10  0.5  ! Nchord   Cspace
TRANSLATE
    33.00000     0.00000     0.00000
#--------------------------------------------------------------
SECTION
    -1.28   0.00000    -2.00000     3.20000     0.000   3   1.5

CONTROL
rudder  1.0  0.4   0.0 0.0 1.0   1.0
#-----------------------
SECTION
    -1.68   0.00000     0.00000     4.20000     0.000   2   0.5

CONTROL
rudder  1.0  0.4   0.0 0.0 1.0   1.0
#-----------------------
SECTION
    -1.5388 0.00000     1.25000     3.847       0.000   8  -1.5

CONTROL
rudder  1.0  0.4   0.0 0.0 1.0   1.0
#-----------------------
SECTION
    -0.72   0.00000     8.50        1.80000     0.000   1   0

CONTROL
rudder  1.0  0.4   0.0 0.0 1.0   1.0

#==============================================================