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


Date:  [Due 28 APR 2006]


PARTICIPANT INFORMATION
-----------------------
               Name: Thomas Scheidegger  
              Email: tes@fluent.com
              Phone: 800-445-4454 x236
            Address: Fluent Inc.
            Address: 10 Cavendish Court 
            Address: Centerra Resource Park 
            Address: Lebanon, NH 03766-1442   


SOLVER INFORMATION
--------------------
        Method Name:  Fluent 6.3
    Basic Algorithm:  unstructured finite-volume, density-based coupled solver (Roe FDS), second-order upwind
   Turbulence Model:  realizable k-epsilon
      Miscellaneous:  

GRID INFORMATION
--------------------
Grid-Generator Name:  unknown, official DPW3 grid (Boeing)
          Grid Type:  multi-block
 


COARSE GRID SIZE            W1        W2
----------------------------------------
              Zones:  
        Field Nodes:  
        Field Cells:       1.51M     1.51M
     Boundary Nodes:  
     Boundary Faces:  
   BL 1st-Cell Size:  
 BL Max-Growth Rate:  
           BL Cells:  
      Miscellaneous: distributed official DPW3 grid (Boeing) 


MEDIUM GRID SIZE            W1        W2
----------------------------------------
              Zones:  
        Field Nodes:  
        Field Cells:       4.03M     4.03
     Boundary Nodes:  
     Boundary Faces:  
   BL 1st-Cell Size:  
 BL Max-Growth Rate:  
           BL Cells:  
      Miscellaneous: distributed official DPW3 grid (Boeing) 


MEDIUM-FINE GRID SIZE       W1        W2
----------------------------------------
              Zones:  
        Field Nodes:
        Field Cells:       8.33M     8.33M 
     Boundary Nodes:  
     Boundary Faces:  
   BL 1st-Cell Size:  
 BL Max-Growth Rate:  
           BL Cells:  
      Miscellaneous: distributed official DPW3 grid (Boeing)   


FINE GRID SIZE              W1        W2
----------------------------------------
              Zones:  
        Field Nodes:
        Field Cells:      14.35    14.35
     Boundary Nodes:  
     Boundary Faces:  
   BL 1st-Cell Size:  
 BL Max-Growth Rate:  
           BL Cells:  
      Miscellaneous: distributed official DPW3 grid (Boeing)   


SOLUTION INFORMATION (typical-fine grid)
--------------------
  Computer Platform:  
       # Processors:  
   Operating System:  
           Compiler:  
       Run Time CPU:  
Run Time Wall-Clock:  
Memory Requirements:  
      Miscellaneous:  



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
     1.51M      0.76      0.5      0.4866  0.02168   0.01539   0.00629   -0.07072
     4.03M      0.76      0.5      0.4864  0.02140   0.01510   0.00630   -0.07006
     8.33M      0.76      0.5      0.4852  0.02101   0.01470   0.00631   -0.06924
    14.35M      0.76      0.5      0.4857  0.02100   0.01469   0.00631   -0.06938

DPW-W2

 GRID_SIZE      MACH     ALPHA    CL_TOT    CD_TOT     CD_PR     CD_SF    CM_TOT
     1.51M      0.76      0.5      0.5081  0.02239   0.01614   0.00625   -0.07088
     4.03M      0.76      0.5      0.5091  0.02196   0.01569   0.00627   -0.07024
     8.33M      0.76      0.5      0.5077  0.02139   0.01511   0.00628   -0.06913
    14.35M      0.76      0.5      0.5080  0.02135   0.01507   0.00628   -0.06915

UPPER-SURFACE TRAILING-EDGE SEPARATION LOCATION

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



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     0.2972  0.01407   0.00767   0.00639   ?.?????   -0.07446
      0.76       0.0     0.4227  0.01817   0.01181   0.00636   ?.?????   -0.07173
      0.76       0.5     0.4864  0.02140   0.01510   0.00630   ?.?????   -0.07006
      0.76       1.0     0.5487  0.02581   0.01959   0.00622   ?.?????   -0.06903
      0.76       1.5     0.6060  0.03136   0.02525   0.00611   ?.?????   -0.06827
      0.76       2.0     0.6555  0.03784   0.03185   0.00599   ?.?????   -0.06705
      0.76       2.5     0.6930  0.04484   0.03899   0.00585   ?.?????   -0.06396
      0.76       3.0     0.7129  0.05173   0.04603   0.00569   ?.?????   -0.05760

DPW-W2

      MACH     ALPHA    CL_TOT    CD_TOT     CD_PR     CD_SF CD-CL2/PA    CM_TOT
      0.76      -1.0     0.3188  0.01486   0.00853   0.00633   ?.?????   -0.07631
      0.76       0.0     0.4392  0.01961   0.01335   0.00626   ?.?????   -0.07258
      0.76       0.5     0.5091  0.02196   0.01569   0.00627   ?.?????   -0.07024
      0.76       1.0     0.5694  0.02636   0.02020   0.00616   ?.?????   -0.06843
      0.76       1.5     0.6182  0.03199   0.02598   0.00601   ?.?????   -0.06580
      0.76       2.0     0.6570  0.03837   0.03252   0.00585   ?.?????   -0.06223
      0.76       2.5     0.6844  0.04505   0.03935   0.00570   ?.?????   -0.05712
      0.76       3.0     0.6988  0.05159   0.04604   0.00555   ?.?????   -0.05068



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.

