Date: 5/5/01 


PARTICIPANT INFORMATION
-----------------------
               Name: Uriel Goldberg & Vedat Akdag 
              Email: ucg@metacomptech.com 
              Phone: (805)371-8755 
            Address: Metacomp Technologies, Inc. 
            Address: 650 Hampshire Rd., #200 
            Address: Westlake Village, CA 91361-2510 


SOLVER INFORMATION
--------------------
        Method Name: CFD++ RANS Solver 
    Basic Algorithm: Finite Volume 
   Turbulence Model: Realizable k-e 
      Miscellaneous: multidimensional interpolation 


CASE 1 PROVIDED GRID USED
Mark one line with an X
--------------------
        Multi-block:  
            Overset:  
  Unstructured node:  
  Unstructured cell:  
      Could not use: X
      Miscellaneous: used Case 2 grid refined for solve-to-wall, 3517440 cells 


GRID INFORMATION FOR CASES 2-4
Leave blank if you used the Case 1 provided grid
--------------------
Grid-Generator Name: ICEM CFD 
          Grid Type: Unstructured hex. 
              Zones: 1 
        Field Nodes: 3309583 
        Field Cells: 3248512 
     Boundary Nodes:  
     Boundary Faces:  121496 
   BL 1st-Cell Size: 0.0001 meter 
 BL Max-Growth Rate: 1.21 - 1.30 
           BL Cells: 10 
      Miscellaneous: Law-of-the-Wall mesh, Y+ = 25 


SOLUTION INFORMATION
--------------------
  Computer Platform: SGI Origin 2000 R12000 300 MHz (comparable to 650 P3)  
       # Processors: 16 
   Operating System: IRIX 6.5 
           Compiler: cc 
       Run Time CPU: 320 Hrs. (128 Hrs.)
Run Time Wall-Clock:  20 Hrs. (  8 Hrs.)
Memory Requirements: 8.1 GB 
      Miscellaneous: times in parentheses are for restart runs 



CASE 1 DATA ON PROVIDED GRID (REQUIRED)
---------------------------------------

      MACH     ALPHA    CL_TOT    CD_TOT     CD_PR     CD_SF    CM_TOT
      0.75    -0.335     0.501   0.03200   0.01740   0.01460   -0.1690


CASE 2 DRAG POLAR DATA (REQUIRED)
---------------------------------

      MACH     ALPHA    CL_TOT    CD_TOT     CD_PR     CD_SF    CM_TOT
      0.75      -3.0     0.183   0.02400   0.00916   0.01490   -0.1750
      0.75      -2.0     0.304   0.02600   0.01120   0.01480   -0.1740
      0.75      -1.0     0.423   0.02940   0.01460   0.01470   -0.1710
      0.75       0.0     0.544   0.03430   0.01970   0.01460   -0.1660
      0.75       1.0     0.663   0.04230   0.02790   0.01430   -0.1570
      0.75       2.0     0.757   0.05470   0.04070   0.01400   -0.1400