#============
Name
Swept Flying Wing
End
#============
Units
L 1.0 ft
T 1.0 s
F 1.0 lb
End
#============
Constant
32.18  0.002378   1115.0
End
#============
Reference
# Sref   Cref   Bref
 216.0   3.00   80.0
#
#  Xmom  Ymom   Zmom
  3.26   0.0    0.125
End
#======================
Weight
#  Nbeam  t     Xp    Yp    Zp      Mg    CDA    Vol   Hx   Hy   Hz
*         1.0   1.0   1.0   1.0     1.0   1.0    1.0   1.   1.   1.
   1      0.0   2.20  0.0   0.0   150.0   0.     0.    0.0  0.0  0.0
End
#============
Ground
#  Nbeam  t     Kground
    1     0.    0
End
#============
Beam 1
Wing
#
   t     chord    x      y      z
* 1.0    1.0     1.0    1.0    1.0
  0.0    3.00    0.0    0.0    0.0
 10.0    2.10    8.0   40.0    0.5
 10.0    2.10    8.0   40.0    0.5
 12.0    1.20    8.2   39.2    3.0
#
   t     Cshell   Nshell    Atshell
* 1.0    0.007    0.007     0.000050
  0.0    0.50     0.50      0.025
  3.0    0.50     0.50      0.015
  3.0    0.375    0.375     0.015
 10.0    0.375    0.375     0.010
 10.0    0.375    0.375     0.010
 11.5    0.375    0.375     0.010
#
   t     alpha    Cm      Cdf
* 1.0    1.0      1.0     1.0   
  0.0    6.0      0.05    0.015
 10.0    6.0      0.05    0.015
 10.0    2.0      0.0     0.015
 11.5    2.0      0.0     0.015
#
  t   twist
* 1.0  0.5
  0.0  0.0
  2.0  0.0
  5.0 -0.2
  7.0 -1.0
  8.5 -2.4
 10.0 -5.0
 10.0 -0.0
 11.5 -0.0
#
  t    dCLdF1   dCMdF1
* 1.0  1.0      1.0    
-11.5  0.0      0.0   
-10.0  0.0      0.0   
-10.0  0.07    -0.03  
 -9.0  0.07    -0.03  
 -6.0  0.07    -0.03  
 -6.0  0.0      0.0
  6.0  0.0      0.0
  6.0 -0.07     0.03  
  9.0 -0.07     0.03  
 10.0 -0.07     0.03  
 10.0  0.0      0.0   
 11.5  0.0      0.0   
#
  t    dCLdF2   dCMdF2
* 1.0  1.0      1.0
  0.0  0.07    -0.01
  4.0  0.07    -0.01
  4.0  0.0      0.0 
 10.0  0.0      0.0 
 10.0  0.0      0.0
 11.5  0.0      0.0
#
  t    dCLdF3   dCMdF3
* 1.0  1.0      1.0
-11.5  0.07    -0.03  
-10.0  0.07    -0.03  
-10.0  0.0      0.0   
 -9.0  0.0      0.0
 -6.0  0.0      0.0
 -6.0  0.0      0.0
  6.0  0.0      0.0
  6.0  0.0      0.0   
  9.0  0.0      0.0   
 10.0  0.0      0.0   
 10.0 -0.07    -0.03
 11.5 -0.07    -0.03
#
  t    dCLda
* 1.0  1.0  
  0.0  6.2  
 10.0  6.2  
 10.0  6.2  
 11.5  6.2  
#
  t    CLmax  CLmin
* 1.0  5.0    5.0 
  0.0  1.1   -1.1
 10.0  1.1   -1.1
 10.0  1.1   -1.1
 11.5  1.1   -1.1
#
  t     Xax   Ccg   Cea   Cta 
* 1.0   1.0   0.1   0.1   0.1 
  0.0   0.35  3.00  3.00  3.00
 10.0   0.35  2.10  2.10  2.10
 10.0   0.35  2.10  2.10  2.10
 11.5   0.35  1.40  1.40  1.40
#
   t   EIcc    EInn     GJ
* 1.0  1.2E4   5.0E7    8.0E3
  0.0 180.0    1.0      40.0
  2.0 120.0    0.7      36.0
  4.0  70.0    0.38     30.0
  7.0  33.0    0.17     16.0
 10.0  20.0    0.08      5.0
 10.0  20.0    0.08      5.0
 11.5   5.0    0.02      2.0
#
  t     mg   mgnn
* 1.0  4.0    2.0
  0.0  0.95   1.0
  1.0  0.95   1.0
  1.0  0.75   1.0
  7.5  0.50   1.0
 10.0  0.40   1.0
 10.0  0.40   1.0
 11.5  0.10   1.0
End
#============