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:  		Spalart-Allmaras
      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:  			0.75	0.74
 BL Max-Growth Rate:  				
           BL Cells:  				
      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:  			0.74	0.74
 BL Max-Growth Rate:  				
           BL Cells:  				
      Miscellaneous:  				


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


SOLUTION INFORMATION (typical-fine grid)				
--------------------				
  Computer Platform:  			Opteron Cluster	
       # Processors:  			4	4
   Operating System:  			SLES 9.0 Linux 	
           Compiler:  				
       Run Time CPU:  			36	36
Run Time Wall-Clock:  			9	9
Memory Requirements:  			8320Mb	8320Mb
      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	0.5	0.47394	0.02110	0.01488	0.00622	-0.06752
4204203		0.76	0.5	0.47590	0.02083	0.01465	0.00618	-0.06745
8620123		0.76	0.5	0.47728	0.02059	0.01443	0.00615	-0.0674
14811489	0.76	0.5	0.47697	0.02053	0.01439	0.00615	-0.0674

DPW-W2							

GRID_SIZE	MACH	ALPHA	CL_TOT	CD_TOT	CD_PR	CD_SF	CM_TOT
1602651		0.76	0.5	0.49563	0.02185	0.01568	0.00618	-0.0678
4204203		0.76	0.5	0.49840	0.02147	0.01532	0.00615	-0.0677
8620123		0.76	0.5	0.49857	0.02094	0.01481	0.00613	-0.06689
14811489	0.76	0.5	0.50049	0.02104	0.01492	0.00612	-0.0674

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	0.28775	0.01370	0.00738	0.00632	0.01041	-0.07187
0.76	-0.500	0.34966	0.01543	0.00912	0.00630	0.01057	-0.07081
0.76	0.000	0.41266	0.01768	0.01142	0.00626	0.01090	-0.06915
0.76	0.500	0.47590	0.02083	0.01465	0.00618	0.01182	-0.06745
0.76	1.000	0.53679	0.02510	0.01904	0.00606	0.01364	-0.06613
0.76	1.500	0.59250	0.03050	0.02459	0.00591	0.01653	-0.06499
0.76	2.000	0.64096	0.03688	0.03113	0.00575	0.02053	-0.06361
0.76	2.500	0.67654	0.04387	0.03829	0.00558	0.02566	-0.06049
0.76	3.000	0.69598	0.05123	0.04583	0.00540	0.03196	-0.05530
							
DPW-W2							

MACH	ALPHA	CL_TOT	CD_TOT	CD_PR	CD_SF	CD-CL2/PA	CM_TOT
0.76	-1	0.30973	0.01456	0.00833	0.00624	0.01074	-0.07385
0.76	-0.500	0.36943	0.01672	0.01053	0.00619	0.01129	-0.07248
0.76	0.000	0.42881	0.01926	0.01312	0.00614	0.01194	-0.07007
0.76	0.500	0.49840	0.02147	0.01532	0.00615	0.01159	-0.06767
0.76	1.000	0.55877	0.02575	0.01975	0.00600	0.01333	-0.06591
0.76	1.500	0.60659	0.03126	0.02546	0.00580	0.01662	-0.06312
0.76	2.000	0.64383	0.03756	0.03196	0.00560	0.02107	-0.0595
0.76	2.500	0.67033	0.04443	0.03900	0.00543	0.02655	-0.05511
0.76	3.000	0.68821	0.05176	0.04650	0.00526	0.03291	-0.05089


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.
