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


Date:  [Due 28 APR 2006]


PARTICIPANT INFORMATION
-----------------------
               Name:  Tom Zickuhr
              Email:  tzickuhr@cessna.textron.com
              Phone:  316-831-2810
            Address:  Cessna Aircraft
            Address:  MS 363P
            Address:  PO Box 7704
            Address:  Wichita, KS 67277-7704
            Address:  
            Address:  


SOLVER INFORMATION
--------------------
        Method Name:  NSU3D
    Basic Algorithm:  Unstructured, Mixed elements, Matrix dissipation, Agglomeration Multigrid
   Turbulence Model:  Spalart-Allmaras
      Miscellaneous:  


GRID INFORMATION
--------------------
Grid-Generator Name:  VGRID 3.6
          Grid Type:  Unstructured Tetrahedral


COARSE GRID SIZE            W1        W2
----------------------------------------
              Zones:  
        Field Nodes:    983633    947409
        Field Cells:  
     Boundary Nodes:     35270     33993
     Boundary Faces:  
   BL 1st-Cell Size:    0.0060    0.0060
 BL Max-Growth Rate:       1.2       1.2
          BL Points:    700549    668560
      Miscellaneous:  The first two layers are not constant.


MEDIUM GRID SIZE            W1        W2
----------------------------------------
              Zones:  
        Field Nodes:   2417082   2325884
        Field Cells:  
     Boundary Nodes:     70449     67138
     Boundary Faces:  
   BL 1st-Cell Size:    0.0040    0.0040
 BL Max-Growth Rate:       1.2       1.2
          BL Points:   1464290   1387601
      Miscellaneous:  The first two layers are not constant.


FINE GRID SIZE              W1        W2
----------------------------------------
              Zones:  
        Field Nodes:   6138245   5963713
        Field Cells:  
     Boundary Nodes:    139768    134164
     Boundary Faces:  
   BL 1st-Cell Size:    0.0027    0.0027
 BL Max-Growth Rate:       1.2       1.2
          BL Points:   2985846   2860490
      Miscellaneous:  The first two layers are not constant.


VERY FINE GRID SIZE         W1        W2
----------------------------------------
              Zones:  
        Field Nodes:  12748678  12419567
        Field Cells:  
     Boundary Nodes:    236291    227109
     Boundary Faces:  
   BL 1st-Cell Size:    0.0018    0.0018
 BL Max-Growth Rate:       1.2       1.2
          BL Points:             4978938
      Miscellaneous:  The first two layers are not constant.


SOLUTION INFORMATION (typical-fine grid)
--------------------
  Computer Platform:  Intel Xeon Dual CPU cluster of 16 or 24 nodes
       # Processors:  32 or 48
   Operating System:  GNU/Linux - Centos 3.5
           Compiler:  Intel Fortran v8.1
       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
   983633.      0.76      0.5      0.477   0.02108   0.01490   0.00618   -0.0673
  2417082.      0.76      0.5      0.474   0.02068   0.01457   0.00611   -0.0664
  6138245.      0.76      0.5      0.471   0.02034   0.01432   0.00602   -0.0657
 12748678.      0.76      0.5      0.472   0.02014   0.01419   0.00594   -0.0656

DPW-W2

 GRID_SIZE      MACH     ALPHA    CL_TOT    CD_TOT     CD_PR     CD_SF    CM_TOT
   947409.      0.76      0.5      0.491   0.02106   0.01490   0.00616   -0.0648
  2325884.      0.76      0.5      0.490   0.02062   0.01453   0.00609   -0.0640
  5963713.      0.76      0.5      0.491   0.02043   0.01442   0.00601   -0.0643
 12419567.      0.76      0.5      0.492   0.02030   0.01437   0.00593   -0.0647

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     0.285   0.01370   0.00745   0.00625   0.01047   -0.0712
      0.76       0.0     0.411   0.01756   0.01137   0.00619   0.01084   -0.0683
      0.76       0.5     0.474   0.02068   0.01457   0.00611   0.01174   -0.0664
      0.76       1.0     0.536   0.02496   0.01897   0.00599   0.01353   -0.0651
      0.76       1.5     0.592   0.03042   0.02459   0.00583   0.01648   -0.0641
      0.76       2.0     0.641   0.03691   0.03126   0.00565   0.02056   -0.0630
      0.76       2.5     0.681   0.04408   0.03860   0.00548   0.02563   -0.0609
      0.76       3.0     0.695   0.05086   0.04556   0.00530   0.03164   -0.0533

DPW-W2

      MACH     ALPHA    CL_TOT    CD_TOT     CD_PR     CD_SF CD-CL2/PA    CM_TOT
      0.76      -1.0     0.299   0.01424   0.00806   0.00618   0.01068   -0.0708
      0.76       0.0     0.420   0.01870   0.01262   0.00608   0.01168   -0.0670
      0.76       0.5     0.490   0.02062   0.01453   0.00609   0.01107   -0.0640
      0.76       1.0     0.550   0.02487   0.01894   0.00593   0.01283   -0.0622
      0.76       1.5     0.597   0.03038   0.02468   0.00570   0.01620   -0.0593
      0.76       2.0     0.638   0.03703   0.03154   0.00549   0.02083   -0.0572
      0.76       2.5     0.669   0.04408   0.03877   0.00531   0.02627   -0.0541
      0.76       3.0     0.677   0.05074   0.04560   0.00514   0.03250   -0.0473



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.

