DPW-III DLR-F6 CASE-1 Data Form
-------------------------------

Date:  [ 28 APR 2006]

PARTICIPANT INFORMATION
-----------------------
               Name:  Alaa Elmiligui - Steve Massey - Khaled Abdol Hamid
              Email:  aelmiligui@asm-usa.com
              Phone:  757-865-7093 ext 314
            Address:  Analytical Services & Materials, Inc
            Address:  107 Research Drive
            Address:  Hampton, Virginia 23666
            Address:
            Address:
            Address:

SOLVER INFORMATION
--------------------
        Method Name:  PAB3D
    Basic Algorithm:  Structured Implicit Upwind Finite Volume
   Turbulence Model:  Two Equation Turbulence Model KE
      Miscellaneous:  

GRID INFORMATION
--------------------
Grid-Generator Name: T.J. Kao and N. J. Yu for Ed. Tinoco
          Grid Type: H-type grid

COARSE GRID SIZE            WB       WBF
----------------------------------------
              Zones:       26 
        Field Nodes:      2.6 million
        Field Cells:      2.3 million
     Boundary Nodes:  
     Boundary Faces:  
   BL 1st-Cell Size:  
 BL Max-Growth Rate:  
           BL Cells:  
      Miscellaneous:  


MEDIUM GRID SIZE            WB       WBF
----------------------------------------
              Zones:        38
        Field Nodes:        9.2 million
        Field Cells:        8.1 million
     Boundary Nodes:  
     Boundary Faces:  
   BL 1st-Cell Size:  
 BL Max-Growth Rate:  
           BL Cells:  
      Miscellaneous:  


MEDIUM-FINE GRID SIZE              WB       WBF
----------------------------------------
              Zones: 49 blocks
        Field Nodes: 18 million
        Field Cells: 16 million
     Boundary Nodes:  
     Boundary Faces:  
   BL 1st-Cell Size:  
 BL Max-Growth Rate:  
           BL Cells:  
      Miscellaneous:  

Fine GRID SIZE            WB       WBF
----------------------------------------
              Zones:        58
        Field Nodes:       30.7 million
        Field Cells:       27.2 million
     Boundary Nodes:
     Boundary Faces:
   BL 1st-Cell Size:
 BL Max-Growth Rate:
           BL Cells:
      Miscellaneous:


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

CASE 1.A:  SINGLE-POINT GRID CONVERGENCE STUDY (REQUIRED, FULLY-TURBULENT)
--------------------------------------------------------------------------

WING/BODY

 GRID_SIZE      MACH     ALPHA    CL_TOT    CD_TOT     CD_PR     CD_SF    CM_TOT
  2298880.      0.75    -0.074     0.501   0.03569   0.01951   0.01617  -0.12770
  8080896.      0.75    -0.074     0.501   0.03401   0.01584   0.01818  -0.14290
 15856320.      0.75    -0.067     0.501   0.03226   0.01625   0.01601  -0.14720
 27185664.      0.75    -0.067     0.501   0.03093   0.01493   0.01600  -0.14720

WING/BODY/FX2B-FAIRING

 GRID_SIZE      MACH     ALPHA    CL_TOT    CD_TOT     CD_PR     CD_SF    CM_TOT
  2298880.      0.75     0.039     0.500   0.03565   0.01947   0.01618  -0.12110
  8080896.      0.75     0.095     0.501   0.03395   0.01553   0.01842  -0.13570
 15856320.      0.75     0.095     0.500   0.03106   0.01495   0.01610  -0.13840
 27185664.      0.75     0.095     0.501   0.03095   0.01485   0.01609  -0.13880

SEPARATION BUBBLE GEOMETRY - WING/BODY - FINE GRID

    FS_BUB    BL_BUB   WL_BUB   FS_EYE_W  BL_EYE_W  WL_EYE_W  FS_EYE_B  BL_EYE_B  WL_EYE_B
    221.71    -71.84     -5.59    236.33    -68.90    -10.69    234.47    -66.51     -7.64

SEPARATION BUBBLE GEOMETRY - WING/BODY/FX2B-FAIRING - FINE GRID

    FS_BUB    BL_BUB   WL_BUB   FS_EYE_W  BL_EYE_W  WL_EYE_W  FS_EYE_B  BL_EYE_B  WL_EYE_B
    ???.??    ???.??   ???.??     ???.??    ???.??    ???.??    ???.??    ???.??    ???.??

UPPER-SURFACE TRAILING-EDGE SEPARATION LOCATION

   STATION     Y (m)     Y/BO2   X/C-WB    X/C-WBF
        1.   0.08785     0.150    0.???      0.???
        2.   0.13987     0.239    0.???      0.???
        3.   0.19453     0.331    0.???      0.???
        4.   0.22156     0.377    0.???      0.???
        5.   0.24037     0.411    0.???      0.???
        6.   0.30090     0.514    0.???      0.???
        7.   0.37319     0.638    0.???      0.???
        8.   0.49602     0.847    0.???      0.??? 



CASE 1.B:  DRAG POLAR - MEDIUM GRID (REQUIRED, FULLY-TURBULENT)
---------------------------------------------------------------

WING/BODY

      MACH     ALPHA    CL_TOT    CD_TOT     CD_PR     CD_SF CD-CL2/PA    CM_TOT
      0.75    -3.000     0.153   0.02576   0.00736   0.01840   0.00008   -0.1547
      0.75    -2.000     0.272   0.02743   0.00906   0.01838  -0.00156   -0.1506
      0.75    -1.000     0.391   0.03028   0.01199   0.01829  -0.00412   -0.1472
      0.75    -0.500     0.451   0.03218   0.01392   0.01826  -0.00574   -0.1451
      0.75     0.000     0.510   0.03442   0.01621   0.01820  -0.00755   -0.1425
      0.75     0.500     0.570   0.03717   0.01903   0.01814  -0.00964   -0.1391
      0.75     1.000     0.632   0.04084   0.02277   0.01807  -0.01203   -0.1359
      0.75     1.500     0.695   0.04581   0.02786   0.01795  -0.01467   -0.1330

WING/BODY/FX2B-FAIRING

      MACH     ALPHA    CL_TOT    CD_TOT     CD_PR     CD_SF CD-CL2/PA    CM_TOT
      0.75    -3.000     0.129   0.02537   0.00672   0.01865   0.00029   -0.1473
      0.75    -2.000     0.250   0.02681   0.00818   0.01863  -0.00119   -0.1436
      0.75    -1.000     0.370   0.02951   0.01095   0.01856  -0.00359   -0.1402
      0.75    -0.500     0.429   0.03096   0.01267   0.01829  -0.00514   -0.1392
      0.75     0.000     0.490   0.03346   0.01501   0.01845  -0.00693   -0.1362
      0.75     0.500     0.550   0.03578   0.01759   0.01819  -0.00892   -0.1337
      0.75     1.000     0.613   0.03967   0.02135   0.01832  -0.01127   -0.1298
      0.75     1.500     0.677   0.04462   0.02639   0.01822  -0.01388   -0.1274

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=9.5
* CM_TOT    (F10.4) Total Moment Coefficient.

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

* FS_BUB    (F10.2) Fuselage station at the leading edge of the wing root separation bubble (mm)  (measured on the wing)
* BL_BUB    (F10.2) Buttock line at the outboard edge of the wing root separation bubble (mm)  (measured on the wing)
* WL_BUB    (F10.2) Water line at the top edge of the wing root separation bubble (mm)  (measured on the fuselage)

* FS_EYE_W  (F10.2) Fuselage station at the center of the wing root separation bubble (mm) (measured on the wing)
* BL_EYE_W  (F10.2) Buttock line at the center of the wing root separation bubble (mm) (measured on the wing)
* WL_EYE_W  (F10.2) Water line at the center of the wing root separation bubble (mm)  (measured on the wing)

* FS_EYE_B  (F10.2) Fuselage station at the center of the wing root separation bubble (mm) (measured on the fuselage)
* BL_EYE_B  (F10.2) Buttock line at the center of the wing root separation bubble (mm) (measured on the fuselage)
* WL_EYE_B  (F10.2) Water line at the center of the wing root separation bubble (mm)  (measured on the fuselage)

*    NOTE:  Set side-of-body-separation-bubble-data to 0.000 if no bubble is computed.

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

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



