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


Date:  [Due 11 AUG 2006]


PARTICIPANT INFORMATION
-----------------------
               Name: Murayama Mitsuhiro
              Email: murayama.mitsuhiro@jaxa.jp
              Phone: +81-422-40-1382
            Address: Japan Aerospace Exploration Agency 
            Address: 7-44-1 Jindaiji-Higashi,
            Address: Chofu, Tokyo 182-8522 
            Address: JAPAN
            Address:  
            Address:
Co-authors
                Name: Zhong Lei, Kazuomi Yamamoto, Kentaro Tanaka
                      Tohru Hirai, Ryozo Ito, Hiroaki Ishikawa


SOLVER INFORMATION
--------------------
	Method Name: UPACS v1.4 (in-house code of JAXA) 
    Basic Algorithm: Upwind, cell-centered finite volume, Multi-Block structured 
   Turbulence Model: Menter's SST Model 
      Miscellaneous: Roe's flux difference splitting with MUSCL, 
                     MPI, Matrix-Free Gauss-Seidel implicit method


GRID INFORMATION
--------------------
Grid-Generator Name: Gridgen v15.07
          Grid Type: Point matched structured, multiblock


COARSE GRID SIZE            WB       WBF
----------------------------------------
              Zones:       222       222
        Field Nodes:   3138454   3252638
        Field Cells:   2739621   2842878
     Boundary Nodes:     46905     49144
     Boundary Faces:     42746     44860
   BL 1st-Cell Size:   6.0e-04   6.0e-04 [mm]
 BL Max-Growth Rate:      1.29      1.29
           BL Cells:        27        27
      Miscellaneous:  


MEDIUM GRID SIZE            WB       WBF
----------------------------------------
              Zones:       222       222
        Field Nodes:   9791936  10018583
        Field Cells:   8927196   9138772
     Boundary Nodes:    100247    103002
     Boundary Faces:     94120     96769
   BL 1st-Cell Size:   4.0e-04   4.0e-04 [mm]
 BL Max-Growth Rate:      1.17      1.17
           BL Cells:        40        40
      Miscellaneous:  


FINE GRID SIZE              WB       WBF
----------------------------------------
              Zones:       222       222
        Field Nodes:  29816072  29816072
        Field Cells:  27982776  27982776
     Boundary Nodes:    209247    209247
     Boundary Faces:    200368    200368
   BL 1st-Cell Size:   2.7e-04   2.7e-04 [mm]
 BL Max-Growth Rate:      1.12      1.12
           BL Cells:        60        60
      Miscellaneous:  


SOLUTION INFORMATION (typical-fine grid)
--------------------
  Computer Platform: Fujitsu PrimePower HPC2500, SPARC 64V(1.3GHz, 1792cpu) 
       # Processors: 100 
   Operating System: SunOS 5.8
           Compiler: Fujitsu MPI Fortran 
       Run Time CPU: 71.25 hours per 1 CPU
Run Time Wall-Clock: 185.95 hours per 1 CPU
Memory Requirements: 39.0 Gbytes per 100 CPUs
      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
  2739621.      0.75     0.190     0.500   0.02783   0.01641   0.01142   -0.1454
  8927196.      0.75     
 27982776.      0.75     0.316     0.499   0.02757   0.01579   0.01178   -0.1381

WING/BODY/FX2B-FAIRING

 GRID_SIZE      MACH     ALPHA    CL_TOT    CD_TOT     CD_PR     CD_SF    CM_TOT
  2842878.      0.75    -0.104     0.500   0.02666   0.01499   0.01167   -0.1540
  9138772.      0.75    
 27982776.      0.75     0.006     0.500   0.02642   0.01438   0.01205   -0.1480

SEPARATION BUBBLE GEOMETRY - WING/BODY - (FINE GRID) !!!!!!!!!!!!!!COARSE 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
    131.74      88.45   16.66     237.87     83.74     -8.65    229.18     72.41      8.48

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
      0.00      0.00     0.00       0.00      0.00      0.00      0.00      0.00      0.00

UPPER-SURFACE TRAILING-EDGE SEPARATION LOCATION

   STATION     Y (m)     Y/BO2   X/C-WB    X/C-WBF
        1.   0.08785     0.150    0.804      1.000
        2.   0.13987     0.239    1.000      1.000
        3.   0.19453     0.331    1.000      1.000
        4.   0.22156     0.377    1.000      1.000
        5.   0.24037     0.411    1.000      1.000
        6.   0.30090     0.514    1.000      1.000
        7.   0.37319     0.638    1.000      1.000
        8.   0.49602     0.847    1.000      1.000



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.


