DPW-III DPW-Wing Alone CASE-2 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 - Thin Layer NS
    Basic Algorithm:  		Finite Volume
   Turbulence Model:  		Menter k-w SST
      Miscellaneous:  		


GRID INFORMATION		
--------------------		
Grid-Generator Name:  		ICEM
          Grid Type:  		"Structured Block, Point-to-Point Matched"


COARSE GRID SIZE           			W1	W2
----------------------------------------				
              Zones:  			11	11
        Field Nodes:  			1602651	1602651
        Field Cells:  			1511424	1511424
     Boundary Nodes:  			11675	11675
     Boundary Faces:  			10944	10944
   BL 1st-Cell Size:  			y+ ~0.75	0.74
 BL Max-Growth Rate:  			<1.2	<1.2
           BL Cells:  			16	16
      Miscellaneous:  				


MEDIUM GRID SIZE  			W1	W2
----------------------------------------				
              Zones:  			11	11
        Field Nodes:  			4204203	4204203
        Field Cells:  			4030464	4030464
     Boundary Nodes:  			19619	19619
     Boundary Faces:  			18688	18688
   BL 1st-Cell Size:  			y+~0.74	0.74
 BL Max-Growth Rate:  			<1.2	<1.2
           BL Cells:  			24	24
      Miscellaneous:  				


FINE GRID SIZE          			W1	W2
----------------------------------------				
              Zones:  			11	
        Field Nodes:			8620123	
        Field Cells:  			8331264	
     Boundary Nodes:  			39347	
     Boundary Faces:  			38016	
   BL 1st-Cell Size:  			y+~0.55	
 BL Max-Growth Rate:  			<1.2	
           BL Cells:  			36	
      Miscellaneous:  				


VERY FINE GRID SIZE  			W1	W2
----------------------------------------				
              Zones:  			11	17
        Field Nodes:			14750771	14811489
        Field Cells:  			14346240	14346240
     Boundary Nodes:  			48339	48339
     Boundary Faces:  			46848	46848
   BL 1st-Cell Size:  			y+~0.55	0.55
 BL Max-Growth Rate:  			<1.2	<1.2
           BL Cells:  			72	72
      Miscellaneous:  				


SOLUTION INFORMATION (typical-fine grid)				
--------------------				
  Computer Platform:  			Opteron Cluster	
       # Processors:  			4	4
   Operating System:  			SLES 9.0 Linux 2.6.5	
           Compiler:  			PGI 6.1	
       Run Time CPU:  			44	40
Run Time Wall-Clock:  			11	10
Memory Requirements:  			8329Mb	8329Mb
      Miscellaneous:  				



"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
1602651		0.76	0.500	0.46561	0.02033	0.01440	0.00593	-0.0652
4204203		0.76	0.500	0.46579	0.02012	0.01415	0.00597	-0.0647
8620123		0.76	0.500	0.46407	0.01991	0.01388	0.00603	-0.0639
14811489	0.76	0.500	0.46358	0.01987	0.01384	0.00603	-0.0639
							
DPW-W2							
							
GRID_SIZE	MACH	ALPHA	CL_TOT	CD_TOT	CD_PR	CD_SF	CM_TOT
1602651		0.76	0.500	0.48719	0.02102	0.01513	0.00589	-0.0653
4204203		0.76	0.500	0.48776	0.02067	0.01474	0.00594	-0.0647
8620123		0.76	0.500	0.48543	0.02022	0.01422	0.00599	-0.06328
14811489	0.76	0.500	0.48626	0.02026	0.01426	0.00599	-0.0636

UPPER-SURFACE TRAILING-EDGE SEPARATION LOCATION							

STATION	Y(m)	Y/BO2	X/C-W1	X/C-W2			
1	20	0.026	1.000	1.000			
2	120	0.157	1.000	1.000			
3	220	0.289	1.000	1.000			
4	320	0.420	1.000	1.000			
5	420	0.551	1.000	1.000			
6	520	0.682	1.000	1.000			
7	620	0.814	1.000	1.000			
8	720	0.945	1.000	1.000			



"CASE 2.B:  DRAG POLAR - MEDIUM GRID (REQUIRED, FULLY-TURBULENT)"							
---------------------------------------------------------------							

DPW-W1							

MACH	ALPHA	CL_TOT	CD_TOT	CD_PR	CD_SF	CD-CL2/PA	CM_TOT
0.76	-1	0.27995	0.01323	0.00714	0.00609	0.01011	-0.06949
0.76	-0.500	0.34098	0.01489	0.00882	0.00607	0.01026	-0.0683
0.76	0.000	0.40306	0.01706	0.01103	0.00603	0.01060	-0.0665
0.76	0.500	0.46579	0.02012	0.01415	0.00597	0.01149	-0.0647
0.76	1.000	0.52608	0.02429	0.01842	0.00587	0.01328	-0.0633
0.76	1.500	0.58122	0.02957	0.02382	0.00575	0.01613	-0.0620
0.76	2.000	0.62721	0.03573	0.03011	0.00562	0.02008	-0.0601
0.76	2.500	0.66018	0.04244	0.03699	0.00545	0.02510	-0.0563
0.76	3.000	0.67891	0.04939	0.04412	0.00527	0.03105	-0.0508
							
DPW-W2							
							
MACH	ALPHA	CL_TOT	CD_TOT	CD_PR	CD_SF	CD-CL2/PA	CM_TOT
0.76	-1	0.30142	0.01400	0.00799	0.00601	0.01039	-0.07124
0.76	-0.500	0.36057	0.01607	0.01010	0.00597	0.01090	-0.0698
0.76	0.000	0.41910	0.01854	0.01262	0.00592	0.01155	-0.0672
0.76	0.500	0.48776	0.02067	0.01474	0.00594	0.01121	-0.0647
0.76	1.000	0.54788	0.02482	0.01901	0.00581	0.01288	-0.0628
0.76	1.500	0.59569	0.03027	0.02461	0.00565	0.01615	-0.0601
0.76	2.000	0.63182	0.03643	0.03094	0.00548	0.02055	-0.0563
0.76	2.500	0.65736	0.04307	0.03777	0.00530	0.02588	-0.0517
0.76	3.000	0.67463	0.05003	0.04491	0.00512	0.03192	-0.0471


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.
