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


Date:  3 AUG 2006		


PARTICIPANT INFORMATION		
-----------------------		
               Name:  		Edward N. Tinoco
              Email:  		edward.n.tinoco@boeing.com
              Phone:  		425-234-1147
            Address:  		Boeing Commercial Airplanes
            Address:  		Mail Code 67-LK
            Address:  		P.O. Box 3707
            Address:  		"Seattle, WA 98124"
            Address:  		USA
            Address:  		


SOLVER INFORMATION		
--------------------		
        Method Name:  		CFL3D/Zeus
    Basic Algorithm:  		Finite Volume
   Turbulence Model:  		Menter k-w SST
      Miscellaneous:  		


GRID INFORMATION		
--------------------		
Grid-Generator Name:  		BCA-Advancing Front
          Grid Type:  		"Structured Block, Point-to-Point Matched"


COARSE GRID SIZE   			WB		WBF
----------------------------------------				
              Zones:  			26		26
        Field Nodes:  			"2,635,778"	"2,635,778"
        Field Cells:  			"2,298,880"	"2,298,880"
     Boundary Nodes:  			"24,286"	"24,286"
     Boundary Faces:  			"21,760"	"21,760"
   BL 1st-Cell Size:  			y+~ 0.82	y+~ 0.82
 BL Max-Growth Rate:  			<1.2 		<1.2 
           BL Cells:  			24		24
      Miscellaneous:  				


MEDIUM GRID SIZE     			WB		WB
----------------------------------------				
              Zones:  			38		38
        Field Nodes:  			"9,182,078"	"9,182,078"
        Field Cells:  			"8,080,896"	"8,080,896"
     Boundary Nodes:  			"57,120"	"57,120"
     Boundary Faces:  			"51,456"	"51,456"
   BL 1st-Cell Size:  			y+~0.60		y+~0.60
 BL Max-Growth Rate:  			<1.2 		<1.2 
           BL Cells:  			32		32
      Miscellaneous:  				


FINE GRID SIZE       			WB		WBF
----------------------------------------				
              Zones:  			49		49
        Field Nodes:			"17,977,893"	"17,977,893"
        Field Cells:  			"15,856,320"	"15,856,320"
     Boundary Nodes:  			"90,993"	"90,993"
     Boundary Faces:  			"81,984"	"81,984"
   BL 1st-Cell Size:  			y+~0.50		y+~0.50
 BL Max-Growth Rate:  			<1.2 		<1.2 
           BL Cells:  			40		40
      Miscellaneous:  				
				
VERY FINE GRID SIZE  			WB		WB
----------------------------------------				
              Zones:  			58		58
        Field Nodes:			"30,751,522"	"30,751,522"
        Field Cells:  			"27,185,664"	"27,185,664"
     Boundary Nodes:  			"126,307"	"126,307"
     Boundary Faces:  			"114,208"	"114,208"
   BL 1st-Cell Size:  			y+~0.40		y+~0.40
 BL Max-Growth Rate:  			<1.2 		<1.2 
           BL Cells:  			48		48
      Miscellaneous:  				


SOLUTION INFORMATION (typical-fine grid)				
--------------------				
  Computer Platform:  			Opteron Cluster	
       # Processors:  			48		48
   Operating System:  			SLES 9.0 Linux 2.6.5	
           Compiler:  			PGI 6.1	
       Run Time CPU:  			96 hr		110 hr
Run Time Wall-Clock:  			4 hr		4.6 hr
Memory Requirements:  			17680Mb		17680Mb
      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
2635778		0.75	-0.03	0.500	0.02694	0.01520	0.01173	-0.1456
9182078		0.75	0.04	0.500	0.02655	0.01472	0.01183	-0.1419
17977893	0.75	0.044	0.500	0.02647	0.01459	0.01189	-0.1420
30751522	0.75	0.044	0.500	0.02647	0.01453	0.01194	-0.1424
							
WING/BODY/FX2B-FAIRING							
							
GRID_SIZE	MACH	ALPHA	CL_TOT	CD_TOT	CD_PR	CD_SF	CM_TOT
2635778		0.75	0.05	0.500	0.02685	0.01504	0.01181	-0.1411	
9182078		0.75	0.116	0.500	0.02643	0.01448	0.01195	-0.1380	
17977893	0.75	0.117	0.500	0.02637	0.01436	0.01202	-0.1379	
30751522	0.75	0.117	0.500	0.02641	0.01434	0.01207	-0.1381	

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
208.0	83.5	0.5	235.0		73.5		surface		242.0		surface		-3.5

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	0.15	1.000	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	0.3009	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
0.75	-3	0.145	0.01824	0.00625	0.01199	0.01754	-0.1583
0.75	-2	0.263	0.01981	0.00783	0.01198	0.01749	-0.1535
0.75	-1	0.380	0.02251	0.01057	0.01194	0.01766	-0.1486
0.75	-0.5	0.437	0.02427	0.01239	0.01189	0.01787	-0.1454
0.75	0	0.495	0.02633	0.01450	0.01184	0.01812	-0.1422
0.75	0.5	0.553	0.02895	0.01716	0.01178	0.01869	-0.1387
0.75	1	0.617	0.03242	0.02078	0.01165	0.01964	-0.1351
0.75	1.5	0.680	0.03726	0.02576	0.01151	0.02175	-0.1325
							
							
WING/BODY/FX2B-FAIRING							
							
MACH	ALPHA	CL_TOT	CD_TOT	CD_PR	CD_SF	CD-CL2/PA	CM_TOT
0.75	-3	0.126	0.01788	0.00579	0.01209	0.01735	-0.1521
0.75	-2	0.247	0.01936	0.00726	0.01210	0.01732	-0.1480
0.75	-1	0.367	0.02198	0.00992	0.01206	0.01748	-0.1438
0.75	-0.5	0.426	0.02375	0.01173	0.01202	0.01767	-0.1414
0.75	0	0.486	0.02585	0.01389	0.01196	0.01794	-0.1385
0.75	0.5	0.547	0.02856	0.01664	0.01192	0.01853	-0.1352
0.75	1	0.612	0.03205	0.02025	0.01180	0.01951	-0.1326
0.75	1.5	0.676	0.03701	0.02536	0.01166	0.02168	-0.1302
							
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.
