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


Date:  [Due 28 APR 2006]


PARTICIPANT INFORMATION
-----------------------
               Name:     Dimitri Mavriplis
              Email:     mavripl@uwyo.edu
              Phone:     307-766-2868
            Address:     Department of Mechanical Engineering
            Address:     University of Wyoming
            Address:     1000 E. University Ave.
            Address:     Laramie WY 82072
            Address:     USA
            Address:
                                                                                                                       
                                                                                                                       
SOLVER INFORMATION
--------------------
        Method Name:    NSU3D
    Basic Algorithm:    Unstructured, mixed elements, multigrid
   Turbulence Model:    Spalart-Allmaras
      Miscellaneous:
                                                                                                                       
                                                                                                                       
GRID INFORMATION
--------------------
Grid-Generator Name:    VGRID
          Grid Type:    LaRC Node-Based Unstructured Grid Set (merged into mixed elements)


COARSE GRID SIZE            W1        W2
----------------------------------------
              Zones:           1          1
        Field Nodes:     1818508    1894205
        Field Cells:     5886795    6059851
     Boundary Nodes:       52243      54436
     Boundary Faces:      100768     104996
   BL 1st-Cell Size:  
 BL Max-Growth Rate:  
           BL Cells:     2394517    2531620 (prisms)
      Miscellaneous: LaRC Node-Based Unstructured Grid Set (merged into mixed elements)


MEDIUM GRID SIZE            W1        W2
----------------------------------------
              Zones:          1           1
        Field Nodes:     4495117    4678575
        Field Cells:     1601624   16546262
     Boundary Nodes:      110866     115537
     Boundary Faces:      216293     225461
   BL 1st-Cell Size:  
 BL Max-Growth Rate:  
           BL Cells:     5203102    5475195 (prisms)
      Miscellaneous: LaRC Node-Based Unstructured Grid Set (merged into mixed elements)


FINE GRID SIZE              W1        W2
----------------------------------------
              Zones:          1           1
        Field Nodes:   11492625    11933637
        Field Cells:   45223548    46526874
     Boundary Nodes:     235347      245871
     Boundary Faces:     462773      483520
   BL 1st-Cell Size:  
 BL Max-Growth Rate:  
           BL Cells:   11170104   11822866 (prisms)
      Miscellaneous: LaRC Node-Based Unstructured Grid Set (merged into mixed elements)


VERY FINE GRID SIZE         W1        W2
----------------------------------------
              Zones:          1           1
        Field Nodes:   36956019    38515559
        Field Cells:  158693482   163482463
     Boundary Nodes:     611352      646905
     Boundary Faces:    1210687     1281320
   BL 1st-Cell Size:  
 BL Max-Growth Rate:  
           BL Cells:   29317606    31531608 (prisms)
      Miscellaneous: LaRC Node-Based Unstructured Grid Set (merged into mixed elements)


SOLUTION INFORMATION (typical-fine grid) --> ~ 11M to 12M pts
--------------------
  Computer Platform:   NASA Columbia
       # Processors:   96 
   Operating System:   Linux
           Compiler:   ifort
       Run Time CPU:
Run Time Wall-Clock:   45 minutes to 75 minutes
Memory Requirements:   34 Gbytes
      Miscellaneous:   Time variance due to different convergence rates



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
   1818508      0.76      0.5      0.470   0.02097   0.01482   0.00615   -0.0660
   4495117      0.76      0.5      0.465   0.02019   0.01410   0.00609   -0.0643
  11492625      0.76      0.5      0.461   0.01976   0.01372   0.00603   -0.0632
  36956019      0.76      0.5      0.457   0.01943   0.01346   0.00597   -0.0624
                                                                                                                   
DPW-W2
                                                                                                                   
 GRID_SIZE      MACH     ALPHA    CL_TOT    CD_TOT     CD_PR     CD_SF    CM_TOT
   1882672      0.76      0.5      0.490   0.02122   0.01510   0.00612   -0.0651
   4658853      0.76      0.5      0.485   0.02038   0.01431   0.00607   -0.0630
  11903329      0.76      0.5      0.480   0.01988   0.01386   0.00602   -0.0615
  38462630      0.76      0.5      0.476   0.01952   0.01357   0.00595   -0.0607


UPPER-SURFACE TRAILING-EDGE SEPARATION LOCATION  (FINE GRID: ~11-12M pts)
**Defined as location where cf in direction normal to trailing edge line becomes negative**
   STATION     Y(mm)     Y/BO2   X/C-W1     X/C-W2
        1.       20.     0.026    0.987      0.989
        2.      120.     0.157    0.987      0.9995
        3.      220.     0.289    0.994      0.995
        4.      320.     0.420    0.9996     0.985
        5.      420.     0.551    0.9996     0.981
        6.      520.     0.682    0.9996     0.988
        7.      620.     0.814    0.9996     0.9998
        8.      720.     0.945    0.9999     0.9998



CASE 2.B:  DRAG POLAR - FINE   GRID (REQUIRED, FULLY-TURBULENT) <--Actually done for fine grid (not med grid)
---------------------------------------------------------------

DPW-W1

      MACH     ALPHA    CL_TOT    CD_TOT     CD_PR     CD_SF CD-CL2/PA    CM_TOT
      0.76      -1.0     0.274   0.01311   0.00694   0.00616   0.01012   -0.0683
      0.76       0.0     0.398   0.01678   0.01067   0.00611   0.01048   -0.0651
      0.76       0.5     0.461   0.01976   0.01372   0.00603   0.01130   -0.0632
      0.76       1.0     0.521   0.02384   0.01793   0.00591   0.01304   -0.0615
      0.76       1.5     0.576   0.02904   0.02327   0.00577   0.01584   -0.0600
      0.76       2.0     0.623   0.03520   0.02960   0.00560   0.01976   -0.0580
      0.76       2.5     0.655   0.04199   0.03658   0.00541   0.02492   -0.0541
      0.76       3.0     0.653   0.04901   0.04382   0.00519   0.03204   -0.0477

DPW-W2

      MACH     ALPHA    CL_TOT    CD_TOT     CD_PR     CD_SF CD-CL2/PA    CM_TOT
      0.76      -1.0     0.292   0.01368   0.00757   0.00610   0.01029   -0.0686
      0.76       0.0     0.411   0.01802   0.01201   0.00601   0.01130   -0.0647
      0.76       0.5     0.480   0.01988   0.01386   0.00602   0.01071   -0.0615
      0.76       1.0     0.541   0.02398   0.01811   0.00587   0.01233   -0.0598
      0.76       1.5     0.587   0.02926   0.02360   0.00566   0.01555   -0.0564
      0.76       2.0     0.623   0.03547   0.03002   0.00545   0.02003   -0.0526
      0.76       2.5     0.647   0.04258   0.03732   0.00526   0.02592   -0.0489
      0.76       3.0     0.650   0.05018   0.04509   0.00509   0.03337   -0.0454


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.

