Date: 7 May 2001 PARTICIPANT INFORMATION ----------------------- Name: Don W. Kinsey Email: don.Kinsey@wpafb.af.mil Phone: (937) 255-4305 Address: AFRL/VAAC Address: 2210 Eighth St. Address: Wright-Patterson AFB OH 45433 SOLVER INFORMATION -------------------- Method Name: Cobalt60 Basic Algorithm: Godunov Turbulence Model: Spalart-Allmaras Miscellaneous: Unstructured, arbitrary cell type CASE 1 PROVIDED GRID USED Mark one line with an X -------------------- Multi-block: X - converted to a single block in Cobalt format Overset: Unstructured node: Unstructured cell: Could not use: GRID INFORMATION FOR CASES 2-4 Leave blank if you used the Case 1 provided grid -------------------- Grid-Generator Name: Grid Type: Zones: Field Nodes: Field Cells: Boundary Nodes: Boundary Faces: BL 1st-Cell Size: BL Max-Growth Rate: BL Cells: Miscellaneous: SOLUTION INFORMATION -------------------- Computer Platform: IBM Power 3 SMP # Processors: 64 Operating System: SMP AIX Compiler: IBM:XL Fortran 90 Run Time CPU: 62000 sec X 64 cpu = 3968000 sec Run Time Wall-Clock: 62000 sec Memory Requirements: 10.06 Gb (double precision) Miscellaneous: CASE 1 DATA ON PROVIDED GRID (REQUIRED) --------------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -0.59 0.4997 0.02282 0.01507 0.00721 -0.1861 CASE 2 DRAG POLAR DATA (REQUIRED) --------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -3.0 0.214 0.01429 0.00704 0.00724 -0.1908 0.75 -2.0 0.332 0.01682 0.00958 0.00724 -0.1899 0.75 -1.0 0.451 0.02068 0.01304 0.00722 -0.1874 0.75 0.0 0.569 0.02579 0.01864 0.00715 -0.1818 0.75 1.0 0.690 0.03484 0.02779 0.00705 -0.1749 0.75 2.0 0.765 0.04771 0.04095 0.00676 -0.1507 CASE 3 DRAG RISE DATA (OPTIONAL) -------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.50 ?.??? 0.500 ?.????? ?.????? ?.????? ?.???? 0.60 ?.??? 0.500 ?.????? ?.????? ?.????? ?.???? 0.70 ?.??? 0.500 ?.????? ?.????? ?.????? ?.???? 0.75 -0.590 0.4997 0.02282 0.01507 0.00721 -0.1861 0.76 ?.??? 0.500 ?.????? ?.????? ?.????? ?.???? 0.77 ?.??? 0.500 ?.????? ?.????? ?.????? ?.???? 0.78 ?.??? 0.500 ?.????? ?.????? ?.????? ?.???? 0.80 ?.??? 0.500 ?.????? ?.????? ?.????? ?.???? CASE 4 ADDITIONAL DRAG RISE DATA (OPTIONAL) ------------------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.50 ?.??? 0.400 ?.????? ?.????? ?.????? ?.???? 0.60 ?.??? 0.400 ?.????? ?.????? ?.????? ?.???? 0.70 ?.??? 0.400 ?.????? ?.????? ?.????? ?.???? 0.75 ?.??? 0.400 ?.????? ?.????? ?.????? ?.???? 0.76 ?.??? 0.400 ?.????? ?.????? ?.????? ?.???? 0.77 ?.??? 0.400 ?.????? ?.????? ?.????? ?.???? 0.78 ?.??? 0.400 ?.????? ?.????? ?.????? ?.???? 0.80 ?.??? 0.400 ?.????? ?.????? ?.????? ?.???? MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.50 ?.??? 0.600 ?.????? ?.????? ?.????? ?.???? 0.60 ?.??? 0.600 ?.????? ?.????? ?.????? ?.???? 0.70 ?.??? 0.600 ?.????? ?.????? ?.????? ?.???? 0.75 ?.??? 0.600 ?.????? ?.????? ?.????? ?.???? 0.76 ?.??? 0.600 ?.????? ?.????? ?.????? ?.???? 0.77 ?.??? 0.600 ?.????? ?.????? ?.????? ?.???? 0.78 ?.??? 0.600 ?.????? ?.????? ?.????? ?.???? 0.80 ?.??? 0.600 ?.????? ?.????? ?.????? ?.???? 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. * CM_TOT (F10.4) Total Moment Coefficient. Date: 07 May, 2001 PARTICIPANT INFORMATION ----------------------- Name: Don W. Kinsey Email: Don.Kinsey@wpafb.af.mil Phone: (937) 255-4305 Address: AFRL/VAAC Address: 2210 Eighth Street Address: Wright-Patterson AFB, OH 45433 SOLVER INFORMATION -------------------- Method Name: Cobalt60 Basic Algorithm: Godunov Turbulence Model: Spalart-Allmaras Miscellaneous: CASE 1 PROVIDED GRID USED Mark one line with an X -------------------- Multi-block: Overset: Unstructured node: Unstructured cell: X Could not use: GRID INFORMATION FOR CASES 2-4 Leave blank if you used the Case 1 provided grid -------------------- Grid-Generator Name: Grid Type: Zones: Field Nodes: Field Cells: Boundary Nodes: Boundary Faces: BL 1st-Cell Size: BL Max-Growth Rate: BL Cells: Miscellaneous: SOLUTION INFORMATION -------------------- Computer Platform: Beowulf Cluster # Processors: 64 Operating System: Linux Compiler: Portland Group Run Time CPU: 52000 sec X 64 cpu = 3328000 sec Run Time Wall-Clock: 52000 sec Memory Requirements: 6.38 Gb (double precision) Miscellaneous: CASE 1 DATA ON PROVIDED GRID (REQUIRED) --------------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -0.711 0.5001 0.02257 0.01758 0.00499 -0.1888 CASE 2 DRAG POLAR DATA (REQUIRED) --------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -3.0 0.226 0.01502 0.00981 0.00522 -0.1912 0.75 -2.0 0.345 0.01732 0.01224 0.00508 -0.1909 0.75 -1.0 0.465 0.02113 0.01612 0.00502 -0.1898 0.75 0.0 0.586 0.02681 0.02184 0.00497 -0.1851 0.75 1.0 0.706 0.03638 0.03146 0.00492 -0.1793 0.75 2.0 0.808 0.05097 0.04618 0.00479 -0.1688 CASE 3 DRAG RISE DATA (OPTIONAL) -------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.50 ?.??? 0.500 ?.????? ?.????? ?.????? ?.???? 0.60 ?.??? 0.500 ?.????? ?.????? ?.????? ?.???? 0.70 ?.??? 0.500 ?.????? ?.????? ?.????? ?.???? 0.75 ?.??? 0.500 ?.????? ?.????? ?.????? ?.???? 0.76 ?.??? 0.500 ?.????? ?.????? ?.????? ?.???? 0.77 ?.??? 0.500 ?.????? ?.????? ?.????? ?.???? 0.78 ?.??? 0.500 ?.????? ?.????? ?.????? ?.???? 0.80 ?.??? 0.500 ?.????? ?.????? ?.????? ?.???? CASE 4 ADDITIONAL DRAG RISE DATA (OPTIONAL) ------------------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.50 ?.??? 0.400 ?.????? ?.????? ?.????? ?.???? 0.60 ?.??? 0.400 ?.????? ?.????? ?.????? ?.???? 0.70 ?.??? 0.400 ?.????? ?.????? ?.????? ?.???? 0.75 ?.??? 0.400 ?.????? ?.????? ?.????? ?.???? 0.76 ?.??? 0.400 ?.????? ?.????? ?.????? ?.???? 0.77 ?.??? 0.400 ?.????? ?.????? ?.????? ?.???? 0.78 ?.??? 0.400 ?.????? ?.????? ?.????? ?.???? 0.80 ?.??? 0.400 ?.????? ?.????? ?.????? ?.???? MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.50 ?.??? 0.600 ?.????? ?.????? ?.????? ?.???? 0.60 ?.??? 0.600 ?.????? ?.????? ?.????? ?.???? 0.70 ?.??? 0.600 ?.????? ?.????? ?.????? ?.???? 0.75 ?.??? 0.600 ?.????? ?.????? ?.????? ?.???? 0.76 ?.??? 0.600 ?.????? ?.????? ?.????? ?.???? 0.77 ?.??? 0.600 ?.????? ?.????? ?.????? ?.???? 0.78 ?.??? 0.600 ?.????? ?.????? ?.????? ?.???? 0.80 ?.??? 0.600 ?.????? ?.????? ?.????? ?.???? 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. * CM_TOT (F10.4) Total Moment Coefficient.