DPW-III DPW-Wing Alone CASE-2 Data Form
-------------------------------


Date:  28 APR 2006


PARTICIPANT INFORMATION
-----------------------
               Name:  Tony Sclafani
              Email:  tony.sclafani@boeing.com
              Phone:  714-896-1074
            Address:  The Boeing Company
            Address:  5301 Bolsa Avenue
            Address:  Huntington Beach, CA
            Address:  92647

SOLVER INFORMATION
--------------------
        Method Name:  OVERFLOW MPI v2.0z
    Basic Algorithm:  Roe Upwind
   Turbulence Model:  Spalart-Allmaras 1-equation
      Miscellaneous:  MPI - Message Passing Interface


GRID INFORMATION
--------------------
Grid-Generator Name:  Surface Grids - ZONI3G/SURGRD,  Volume Grids - HYPGEN/LEGRID/PEGASUS5
          Grid Type:  Structured Overset


COARSE GRID SIZE            W1        W2
----------------------------------------
              Zones:         5         5
        Field Nodes:  
        Field Cells:  
     Boundary Nodes:  
     Boundary Faces:  
   BL 1st-Cell Size:   0.00055   0.00055
 BL Max-Growth Rate:      1.29      1.29
           BL Cells:  
      Miscellaneous:  


MEDIUM GRID SIZE            W1        W2
----------------------------------------
              Zones:         5         5
        Field Nodes:  
        Field Cells:  
     Boundary Nodes:  
     Boundary Faces:  
   BL 1st-Cell Size:   0.00038   0.00038
 BL Max-Growth Rate:      1.19      1.19
           BL Cells:  
      Miscellaneous:  


FINE GRID SIZE              W1        W2
----------------------------------------
              Zones:         5         5 
        Field Nodes:
        Field Cells:  
     Boundary Nodes:  
     Boundary Faces:  
   BL 1st-Cell Size:   0.00025   0.00025  
 BL Max-Growth Rate:      1.12      1.12
           BL Cells:  
      Miscellaneous:  


VERY FINE GRID SIZE         W1        W2
----------------------------------------
              Zones:         5         5
        Field Nodes:
        Field Cells:  
     Boundary Nodes:  
     Boundary Faces:  
   BL 1st-Cell Size:   0.00016   0.00016  
 BL Max-Growth Rate:      1.08      1.08
           BL Cells:  
      Miscellaneous:  


SOLUTION INFORMATION (typical-fine grid)
--------------------
  Computer Platform: Linux PC Cluster 
       # Processors: extra-fine 16; fine 12; medium 2; coarse 2 
   Operating System:  
           Compiler:  
       Run Time CPU:  
Run Time Wall-Clock:  
Memory Requirements:  
      Miscellaneous: The 3.0 alpha solutions had a large amount of oscillation in
		     the force and moment histories.



CASE 2.A:  SINGLE-POINT GRID CONVERGENCE STUDY (REQUIRED, FULLY-TURBULENT)
--------------------------------------------------------------------------

    DPW-W1

 GRID_SIZE      MACH     ALPHA    CL_TOT    CD_TOT     CD_PR     CD_SF    CM_TOT
  1442285.      0.76       0.5     0.469   0.02074   0.01476   0.00598   -0.0660
  4856149.      0.76       0.5     0.474   0.02029   0.01432   0.00598   -0.0667
 16265909.      0.76       0.5     0.478   0.02023   0.01424   0.00598   -0.0675
 55014321.      0.76       0.5     0.480   0.02022   0.01423   0.00599   -0.0679

    DPW-W2

 GRID_SIZE      MACH     ALPHA    CL_TOT    CD_TOT     CD_PR     CD_SF    CM_TOT
  1442285.      0.76       0.5     0.492   0.02118   0.01523   0.00595   -0.0658
  4856149.      0.76       0.5     0.497   0.02063   0.01468   0.00595   -0.0664
 16265909.      0.76       0.5     0.500   0.02048   0.01453   0.00595   -0.0669
 55014321.      0.76       0.5     0.501   0.02046   0.01450   0.00596   -0.0671

UPPER-SURFACE TRAILING-EDGE SEPARATION LOCATION

   STATION     Y(mm)     Y/BO2    X/C-W1    X/C-W2
        1.       20.     0.026     1.000     1.000
        2.      120.     0.157     1.000     1.000
        3.      220.     0.289     1.000     1.000
        4.      320.     0.420     1.000     1.000
        5.      420.     0.551     1.000     1.000
        6.      520.     0.682     1.000     1.000
        7.      620.     0.814     1.000     1.000
        8.      720.     0.945     1.000     1.000 



CASE 2.B:  DRAG POLAR - MEDIUM GRID (REQUIRED, FULLY-TURBULENT)
---------------------------------------------------------------

    DPW-W1

      MACH     ALPHA    CL_TOT    CD_TOT     CD_PR     CD_SF CD-CL2/PA    CM_TOT
      0.76      -1.0     0.287   0.01329   0.00717   0.00612   0.01002   -0.0713
      0.76       0.0     0.411   0.01717   0.01111   0.00606   0.01044   -0.0686
      0.76       0.5     0.474   0.02029   0.01432   0.00598   0.01134   -0.0667
      0.76       1.0     0.536   0.02458   0.01871   0.00586   0.01316   -0.0655
      0.76       1.5     0.594   0.03014   0.02441   0.00573   0.01608   -0.0652
      0.76       2.0     0.647   0.03676   0.03118   0.00558   0.02012   -0.0649
      0.76       2.5     0.688   0.04413   0.03872   0.00541   0.02528   -0.0634
      0.76       3.0     0.711   0.05193   0.04670   0.00522   0.03182   -0.0594

    DPW-W2

      MACH     ALPHA    CL_TOT    CD_TOT     CD_PR     CD_SF CD-CL2/PA    CM_TOT
      0.76      -1.0     0.306   0.01409   0.00804   0.00604   0.01035   -0.0729
      0.76       0.0     0.425   0.01865   0.01271   0.00594   0.01146   -0.0690
      0.76       0.5     0.497   0.02063   0.01468   0.00595   0.01082   -0.0664
      0.76       1.0     0.557   0.02496   0.01915   0.00581   0.01262   -0.0647
      0.76       1.5     0.608   0.03073   0.02512   0.00562   0.01601   -0.0629
      0.76       2.0     0.650   0.03748   0.03206   0.00542   0.02065   -0.0606
      0.76       2.5     0.682   0.04495   0.03972   0.00523   0.02643   -0.0579
      0.76       3.0     0.702   0.05288   0.04781   0.00507   0.03326   -0.0555



NOTES:
------
* Information lines are 80 characters long.
* Information blocks allow free-form miscellaneous information.

* MACH      (F10.2) Mach Number.
* ALPHA     (F10.3) Angle of Attack in Degrees.

* CL_TOT    (F10.3) Total Lift Coefficient.
* CD_TOT    (F10.5) Total Drag Coefficient.
* CD_PR     (F10.5) Surface-Pressure Integrated Drag Coefficient.
* CD_SF     (F10.5) Skin-Friction Integrated Drag Coefficient.
* CD-CL2/PA (F10.5) CD_TOT - (CL_TOT*CL_TOT)/(PI*AR)
                    Note: AR=8.0
* CM_TOT    (F10.4) Total Moment Coefficient.

* GRID_SIZE (F10.0) Number of grid nodes or cells

* STATION   (F10.0) Wing station number [Consistent with Cp-data stations].
* Y/BO2     (F10.3) Wing semi-span fraction of station data.
* X/C-W1    (F10.3) Upper-surface trailing-edge separation location for DPW-W1 geometry.
* X/C-W2    (F10.3) Upper-surface trailing-edge separation location for DPW-W2 geometry.

     NOTE:  Set X/C-W* to 1.000 if no TE separation is detected in solution.

