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


Date:  September 22, 2006


PARTICIPANT INFORMATION
-----------------------
               Name: Venkat Venkatakrishnan
              Email: venkat.venkatakrishnan@boeing.com
              Phone: (425) 234-3124 
            Address: Boeing Commercial Airplanes 
            Address: P.O. Box 3707, M/S 67-LF 
            Address: Seattle, WA 98124-2207
            Address:  
            Address:  
            Address:  


SOLVER INFORMATION
--------------------
        Method Name: CFD++ 
    Basic Algorithm: Finite volume 
   Turbulence Model: Spalart-Allmaras 
      Miscellaneous:  


GRID INFORMATION
--------------------
Grid-Generator Name: MADCAP, AFLR 
          Grid Type: Unstructured, mixed tet/prism 


COARSE GRID SIZE            WB       WBF  (St. Louis grid)
----------------------------------------
              Zones:        N/A       354 
        Field Nodes:  
        Field Cells:        N/A        3909125
     Boundary Nodes:  
     Boundary Faces:        --       --
   BL 1st-Cell Size:        --       --
 BL Max-Growth Rate:        --       --
           BL Cells:                 2769054 (prisms)
      Miscellaneous:  cell size in mm


MEDIUM GRID SIZE            WB       WBF (St. Louis grid)
----------------------------------------
              Zones:        366       366 
        Field Nodes:  
        Field Cells:      8586991   7762514
     Boundary Nodes:  
     Boundary Faces:        --       184393
   BL 1st-Cell Size:        --       --
 BL Max-Growth Rate:  
           BL Cells:      6593623   5241546 (prisms)
      Miscellaneous:  


FINE GRID SIZE              WB       WBF (St. Louis grid)
----------------------------------------
              Zones:        
        Field Nodes: 
        Field Cells:  33837449  35757495
     Boundary Nodes:  
     Boundary Faces:  508735     495891
   BL 1st-Cell Size:  
 BL Max-Growth Rate:  
           BL Cells:  15674260   16114379 (prisms)
      Miscellaneous:  


SOLUTION INFORMATION (typical-fine grid)
--------------------
  Computer Platform: 64 bit Opteron
       # Processors: 
   Operating System: Linux 
           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	
N/A		0.75	-0.191	0.500	0.0314	0.00000	0.00000	0.0000		
8656991		0.75	-0.195	0.500	0.0304	0.00000	0.00000	0.0000		
33837449	0.75	-0.782	0.500	0.0321	0.00000	0.00000	0.0000		

WING/BODY/FX2B-FAIRING

GRID_SIZE	MACH	ALPHA	CL_TOT	CD_TOT	CD_PR	CD_SF	CM_TOT	
3909125		0.75	-0.072	0.500	0.0298	0.00000	0.00000	0.0000	
7762514	 	0.75	-0.028	0.500	0.0295	0.00000	0.00000	0.0000	
35757495	0.75    -0.036	0.500	0.0294	0.00000	0.00000	0.0000	

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
   

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
    0.000    0.000   0.000     0.000    0.000    0.000    0.000    0.000    0.000

UPPER-SURFACE TRAILING-EDGE SEPARATION LOCATION

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



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
      
WING/BODY/FX2B-FAIRING

      MACH     ALPHA    CL_TOT    CD_TOT     CD_PR     CD_SF CD-CL2/PA    CM_TOT
     


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.

