0.     <t_ini  ) Time     >FLT2DQ\_EPLD3D.INP for Structure EPLD3D <.........
   2.     <t_end  ) interval  ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
   2001   <npoints)          >Above 40 characters for Tecplot legend  <.........
 -40.0    <y0(1) (x1s)  )
   0.0    <y0(2) (x2s)  ) Initial values
   1.00   <y0(3) (x1)   )
   1.00   <y0(4) (x2)   )
  0.057370<m1                 )
  0.046712<m2                 )  Mass matrix (fm > 0 scales mass matrix)
    0.0   <sm>  0.0     <fm   )
    .0000 <d1           ) Damping
    .0000 <d2           )
  41.653  <k1>  0.0     <km   )  Stiffness matrix
 1089.1   <k2                 )
     0.   <kap. . . . . . Spring coupling
     0.   <a0 . . . . . ) Amplitude )
     2.5  <f0 . .[Hz] . ) Frequency )   External force
    0.    <phase.[deg]. ) Phase     )
     1d-05<tol. . . . . . Accuracy  )Method 2 for tol < 1d-07 required)
    1     <method . . . . 1: Adams-Moulton 2: Gear's BDF
   00     <iout06 . . . . Output to screen  06 (no output: 00)
.......... Input for aerodynamic loads *) see note below .......................
  -7080.  <>   0.00   <>    0.50  <>   0.00   <>   0.036  <fs/omred/xdr/ma/scale
 0.001438 <>-0.01317  <CQ11   ****  Optional input for airloads
-0.09942  <>-0.02209  <CQ12
 0.0008807<> 0.011136 <CQ21     1.  omred=0 means: Read CQij
 0.085454 <>-0.012958 <CQ22     2.  omred>0 means: Apply thin plate theory
.......... Flutter calculation in frequency domain *) see note below ...........
     0.36 <x_ref. . . . . Chord length
     1.2  <rho. . . . . . Density
     0.0  <q0_ini . . . . Lower limit for stagnation pressure q0 = abs(fs)
     20   <iflint . . . . Number of intervals for dividing |q0_ini,q0|
      5   <iflplus  . . . Number of intervals of same spacing above q0
      5   <kdist. . . . . Distance in frequency intervals for "strong coupling"
--- End of all input data (Line Required) --------------------------------------
--------------------------------------------------------------------------------

Legend and Comments:

*) The dot in the first column is required

> The >___< signs delimiting an input field are occasionally used as controls
            Do not remove.

> Parameter input in case using thin plate theory (omred > 0)
  - fs . . . . Stagnation pressure q0 in N/m**2 (q0 = |fs| used that case)
  - omred. . . Reduced frequency base on half chord length
  - xdr. . . . Relative pitch axis relative to chord length
  - ma . . . . Mach number correction 1/srqt(1-ma**2) for airloads
  - scale. . . Scale factor for the 2D lift and moment coefficients

> The CQij are taken as aerodynamic loads (omred = 0)
  - The present aerodynamic loads are taken from ZAERO.
  - They are computed for omred=0.2
  - The ZAERO data already include the minus sign for the fluid forces!

> Scaling 2D thin plate theory for the given structure EPLD3D:
  - The eigenvectors in EPLD3D are approximately a = 0.2 at the tip
    Thus, the average from root to tip is about 0.1 (that's all one can do)
    The surface S is  S = 1 m x 0.36 m
  - Thus, an approximate scaling is: scale = S * a/2 = 0.036

*** End of data file ***********************************************************