0.     <t_ini  ) Time     >FLT2DQ.INP - Minimum input file         <.........
  10.     <t_end  ) interval  ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
   2001   <npunkte)          >-------< Input fields
   0.0    <y0(1) (x1s)  )
   0.0    <y0(2) (x2s)  ) Initial values
   0.50   <y0(3) (x1)   )
   0.50   <y0(4) (x2)   )
    1.0   <m1>                )
    1.0   <m2                 )  Mass matrix
    0.1   <sm                 )
   0.00   <d1    ) Damping
   0.00   <d2    )
   100.   <k1>      0.  <km   )  Stiffness matrix
   400.   <k2                 )
     0.   <kap. . . . . . Spring coupling
     0.   <a0 . . . . . ) Amplitude )
     0.   <f0 . .[Hz] . ) Frequency )   External force
     0.   <phase.[deg]. ) Phase     )
     1d-06<tol. . . . . . Accuracy  (Methode 2 for tol < 1d-07)
    1     <method . . . . 1: Adams-Moulton 2: Gear's BDF
   00     <iout06 . . . . Output to screen  06 (no output: 00)
i......... Input for aerodynamic loads  *)
  10.00   <>   0.20   <>    0.50  <>   0.00   <>   0.00   <fs/omred/xdr/ma/scale
*** End of input data
*) Legend
i or or I in first column: Inline 2D thin plate unsteady airloads
. in first column:         External airloads expected (on further lines)
x in first column:         No aerodynamic data expected