Jose's Custom K2 3M SAILPLANE
0.0                      Mach
0     0     0.0          iYsym  iZsym  Zsym
#
1000.0 8.0   125         Sref   Cref   Bref    reference area, chord, span
3.75    0.0   0.0        Xref   Yref   Zref    moment reference location
#
#
#==============================================================
SURFACE
Wing
 5  1.0     Nchord   Cspace
#
YDUPLICATE
     0.00000   reflect image wing about y=0 plane
#
ANGLE
     1.00000   twist angle bias for whole surface
#
#--------------------------------------------------------------
SECTION
#    XLE         YLE         ZLE         chord       angle
     0.00000     0.00000     0.00000     7.625        0.000   7  -2.0
AFIL 0.0 0.8026
mh32.dat
#
SECTION
#    XLE         YLE         ZLE         chord       angle
     0.250       24.0        1.25         7.375      0.000  9  1.0
AFIL 0.0 0.797
mh32.dat
SECTION
#    XLE         YLE         ZLE         chord       angle
     2.75       50.0         4.106        5.18       0.00  5  1.0
AFIL 0.0 0.767
mh32.dat
#
SECTION
#    XLE         YLE         ZLE         chord       angle
     4.25      56.0        4.7728         3.75       0.0  5  1.0
AFIL 0.0 0.7142
mh32.dat
#
SECTION
#    XLE         YLE         ZLE         chord       angle
     5.75       62.0        5.4248         2.8568     0.0  0  0
AFIL 0.0 0.7142
mh32.dat
#
#==============================================================
SURFACE
Flap
4	1.0
YDUPLICATE
	0.0
ANGLE
	1.0
CONTROL
1
F  45.0
#--------------------------------------------------------------
SECTION
#    XLE         YLE         ZLE         chord       angle
     7.6250000     0.00000     0.00000     1.875         0.000   7   -2.0
AFIL 0.763 1.0
mh32.dat
#
SECTION
#    XLE         YLE         ZLE         chord       angle
     7.6250       24.0        1.25        1.875        0.000   7  -2.0
AFIL 0.7567 1.0
MH32.dat
#
#==============================================================
SURFACE
Aileron
4	1.0
YDUPLICATE
	0.0
ANGLE
	1.0
CONTROL
1
A -32.76
SECTION
#    XLE         YLE         ZLE         chord       angle
     7.625       24.0        1.25        1.875        0.0  9   1.0
AFIL 0.797 1.0
mh32.dat
#
SECTION
#    XLE         YLE         ZLE         chord       angle
     7.93        50.0        4.106         1.57       0.00  5  1.0
AFIL 0.767 1.0
mh32.dat
#
SECTION
#    XLE         YLE         ZLE         chord       angle
     8.0         56.0        4.7728        1.5        0.0  5  1.0
AFIL 0.6744 1.0
mh32.dat
##
##==============================================================
SURFACE
Dummy outer aileron
4	1.0
YDUPLICATE
	0.0
ANGLE
	1.0
SECTION
#    XLE         YLE         ZLE         chord       angle
     8.0       56.0        4.7728       1.5        0.0  5  1.0
AFIL 0.7142 1.0
mh32.dat
#
SECTION
#    XLE         YLE         ZLE         chord       angle
     8.428     62.0        5.4248      1.1432      0.00   0  0
AFIL 0.7142 1.0
mh32.dat
#
#==============================================================
SURFACE
Right tail
 5  1.0   Nchord   Cspace
#
YDUPLICATE
     0.00000
#
ANGLE
     0.0000
#
TRANSLATE
#   deltaX       deltaY      deltaZ
    36.75000     0.00000     0.0000      position bias for whole surface
#
#--------------------------------------------------------------
SECTION
     0.00000     0.00000     0.00000     3.75         0.000   7   1.0
SECTION
     1.50        11.97       9.02700    2.5         0.000   1   0
#
#
#==============================================================
SURFACE
Right ruddervator
 5  1.0   Nchord   Cspace
#
YDUPLICATE
     0.00000
#
ANGLE
     0.0000
#
TRANSLATE
#   deltaX       deltaY      deltaZ
    36.750000     0.00000     0.0000      position bias for whole surface
#
CONTROL
2
E  37.68       unit elevator command gives 25 degrees of tail rotation
R  -42.9
#--------------------------------------------------------------
SECTION
     3.75000     0.00000     0.00000     1.5         0.000   7   1.0
SECTION
     4.00        11.97         9.027     1.25        0.000   1   0