========================================================================
     Baseline Structured Over-Set Viscous Grid for the DLR-F4 Configuration
    ========================================================================



 Geometry dimensions:

    Body length:                           1192.0 mm
    Semispan         (BO2):                 585.7 mm
    Reference Chord (Cref):                 141.2 mm
    Wing Ref. area  (Sref):              145400.0 mm^2



 Grid statistics:

    Total viscous-surface points:           54445
    Total grid points:                    3727462
    Total non-blanked grid points:        3231377
    Grid points across the TE base              5
    Farfield boundary is a box ~150 chord lengths away.

    grid    id  jd  kd  surfpts  gridpts  %pts  realpts %real  description
       1    49 273  49    13377   655473  17.6   562499  17.4     fuselage
       2   385  65  49    22209  1226225  32.9  1092327  33.8       collar
       3   385  62  49    15934  1169630  31.4  1038606  32.1         wing
       4    25 141  49     2925   172725   4.6   135219   4.2      wingtip
       5   121  22  43        0   114466   3.1    76840   2.4     fuse_box
       6    67  74  46        0   228068   6.1   168408   5.2     wing_box
       7    75  39  55        0   160875   4.3   157468   4.9   global_box
                          -----  -------        -------
               Totals:    54445  3727462        3231377



 Example Grid-to-Processor Mapping for 3 Processors:

    grid:  1  2  3  4  5  6  7
    proc:  3  1  2  3  3  3  3

    proc    nsize  %size
       1  1092327   33.8
       2  1038606   32.1
       3  1100444   34.1

    Maximum Possible Speed-Up:  2.94


 
 Grid spacings:
 
    Chordwise grid spacing at LE             ~0.10% Local Chord
    Chordwise grid spacing at TE             ~0.12% Local Chord
    Spanwise spacing at Root                 ~1.00% Semispan
    Spanwise spacing at Tip                  ~0.10% Semispan
    Grid spacing at the fuselage nose        ~5.000 mm
    First layer spacing off the wall         ~0.001 mm (Y+ ~1)
    Maximum growth ratio in normal dir       ~1.240



 Grid files:     name                size (byte)

           1)    dlr_f4.overflow.input      5607
           2)    dlr_f4.grid.in        104369096
           3)    dlr_f4.XINTOUT         37604648
           4)    dlr_f4.mixsur.inp          2411
           5)    dlr_f4.mixsur.fmp           780
           6)    dlr_f4.grid.ibi         1533000
           7)    dlr_f4.grid.ptv           21304
           8)    README.grid.info           3737
       
 File description/formats

  1)  dlr_f4.overflow.input:  Example Input deck for OVERFLOW_PVM.
        An ASCII Text file.

  2)  dlr_f4.grid.in:  Over-Set Grid System.
        An IEEE Double-Precision PLOT3D, Unformatted, 3D, Blanked file.

  3)  dlr_f4.XINTOUT:  PEGASUS Grid-Coupling Data.
        An IEEE Double-Precision XINTOUT File.

  4)  dlr_f4.mixsur.inp
        An ASCII Text file, Input for MIXSUR.

  5)  dlr_f4.mixsur.fmp
        An ASCII Text file, Output from MIXSUR.

  6)  dlr_f4.grid.ibi
        An IEEE Double-Precision PLOT3D, Unformatted, 3D, Blanked file.

  7)  dlr_f4.grid.ptv
        An IEEE pseudo-PLOT3D, Unformatted, Integer-Pointer file.

  8)  README.grid.info:  This file.
        An ASCII Text file.



************************************************************************

 For questions/problems, contact

  John C. Vassberg
  The Boeing Company
  MS: C078-0421
  2401 E. Wardlow Road
  Long Beach, CA 90807-5309

  Phone:  (562) 593-9604    
  FAX:    (562) 593-7593   
  E-mail: john.c.vassberg@boeing.com

************************************************************************