0. FLT2DQ\_EPLD3D.INP for Structure EPLD3D <.........
2. Above 40 characters for Tecplot legend <.........
-40.0 0 scales mass matrix)
0.0 0.0 0.0 0.00 <> 0.50 <> 0.00 <> 0.036 -0.01317 -0.02209 0.011136 -0.012958 0 means: Apply thin plate theory
.......... Flutter calculation in frequency domain *) see note below ...........
0.36 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 ***********************************************************