Date: 5/07/01 PARTICIPANT INFORMATION ----------------------- Name: Dimitri Mavriplis Email: dimitri@icase.edu Phone: 757-864-2213 Address: ICASE MS 132C Address: NASA Langley Research Center Address: Hampton, VA 23681 Address: Address: Address: SOLVER INFORMATION -------------------- Method Name: NSU3D Basic Algorithm: Unstructured Multigrid Finite Volume Turbulence Model: Spalart-Allmaras Miscellaneous: CASE 1 PROVIDED GRID USED Mark one line with an X -------------------- Multi-block: Overset: Unstructured node: X 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: Linux Cluster (500Mhz Pentium III) # Processors: 32 Operating System: Red Hat Linux 5.2 Compiler: Portland Group F77 Run Time CPU: 25 seconds/MG Cycle (500 cycles) Run Time Wall-Clock: 3.5 hours Memory Requirements: 3.2 Gbytes Miscellaneous: SOLUTION INFORMATION -------------------- Computer Platform: Origin 2000 # Processors: 64 (400Mhz R12000) Operating System: IRIX Compiler: SGI F77 Run Time CPU: 6 seconds/MG cycle (500 cycles) Run Time Wall-Clock: 50 minutes Memory Requirements: 3.6 Gbytes Miscellaneous: CASE 1 DATA ON PROVIDED GRID (REQUIRED) --------------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -.2405 0.5004 0.02921 0.01684 0.01237 -0.1549 CASE 2 DRAG POLAR DATA (REQUIRED) --------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -3.0 0.1620 0.02108 0.00854 0.01255 -0.1632 0.75 -2.0 0.2845 0.02288 0.01036 0.01252 -0.1618 0.75 -1.0 0.4067 0.02594 0.01347 0.01246 -0.1588 0.75 0.0 0.5307 0.03051 0.01817 0.01233 -0.1532 0.75 1.0 0.6545 0.03831 0.02627 0.01204 -0.1437 0.75 2.0 0.7373 0.05133 0.03975 0.01158 -0.1213 CASE 3 DRAG RISE DATA (OPTIONAL) -------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.50 0.522 0.500 0.02839 0.01535 0.01304 -0.1241 0.60 0.280 0.500 0.02834 0.01550 0.01284 -0.1342 0.70 -0.033 0.500 0.02874 0.01618 0.01256 -0.1466 0.75 -0.244 0.500 0.02920 0.01682 0.01237 -0.1549 0.76 -0.296 0.500 0.02932 0.01699 0.01233 -0.1571 0.77 -0.353 0.500 0.02947 0.01719 0.01229 -0.1596 0.78 -0.415 0.500 0.02972 0.01748 0.01224 -0.1629 0.80 -0.404 0.500 0.03262 0.02060 0.01202 -0.1662 CASE 4 ADDITIONAL DRAG RISE DATA (OPTIONAL) ------------------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.50 -0.518 0.400 0.02506 0.01196 0.01310 -0.1323 0.60 -0.698 0.400 0.02501 0.01211 0.01290 -0.1412 0.70 -0.918 0.400 0.02532 0.01268 0.01264 -0.1520 0.75 -1.055 0.400 0.02577 0.01330 0.01247 -0.1591 0.76 -1.086 0.400 0.02586 0.01343 0.01243 -0.1608 0.77 -1.121 0.400 0.02602 0.01364 0.01238 -0.1628 0.78 -1.152 0.400 0.02635 0.01402 0.01232 -0.1651 0.80 -1.176 0.400 0.02763 0.01545 0.01218 -0.1691 MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.50 1.571 0.600 0.03260 0.01964 0.01297 -0.1150 0.60 1.266 0.600 0.03260 0.01986 0.01274 -0.1260 0.70 0.870 0.600 0.03364 0.02125 0.01239 -0.1383 0.75 0.548 0.600 0.03422 0.02203 0.01220 -0.1487 0.76 0.470 0.600 0.03447 0.02232 0.01215 -0.1519 0.77 0.395 0.600 0.03491 0.02282 0.01209 -0.1556 0.78 0.377 0.600 0.03643 0.02445 0.01199 -0.1573 0.80 0.653 0.600 0.04490 0.03323 0.01166 -0.1497 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: 5/07/01 PARTICIPANT INFORMATION ----------------------- Name: Dimitri Mavriplis Email: dimitri@icase.edu Phone: 757-864-2213 Address: ICASE MS 132C Address: NASA Langley Research Center Address: Hampton, VA 23681 Address: Address: Address: SOLVER INFORMATION -------------------- Method Name: NSU3D Basic Algorithm: Unstructured Multigrid Finite Volume Turbulence Model: Spalart-Allmaras Miscellaneous: CASE 1 PROVIDED GRID USED Mark one line with an X -------------------- Multi-block: 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: Unstructured node Zones: Field Nodes: 13,182,480 Field Cells: 77,494,416 Boundary Nodes: 193,356 Boundary Faces: 386,696 BL 1st-Cell Size: BL Max-Growth Rate: BL Cells: Miscellaneous: Subdivision by 8 of baseline workshop "Unstructured node" grid SOLUTION INFORMATION -------------------- Computer Platform: Origin 2000 # Processors: 128 (400Mhz R12000) Operating System: IRIX Compiler: SGI F77 Run Time CPU: 30 seconds / MG cycle for 500 cycles Run Time Wall-Clock: 4 hours Memory Requirements: 27 Gbytes Miscellaneous: CASE 1 DATA ON PROVIDED GRID (REQUIRED) --------------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -.367 0.5003 0.02815 0.01537 0.01278 -0.1657 CASE 2 DRAG POLAR DATA (REQUIRED) --------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -3.0 0.1795 0.02026 0.00731 0.01296 -0.1742 0.75 -2.0 0.3015 0.02225 0.00932 0.01293 -0.1725 0.75 -1.0 0.4226 0.02542 0.01257 0.01286 -0.1691 0.75 0.0 0.5459 0.03011 0.01740 0.01271 -0.1630 0.75 1.0 0.6746 0.03830 0.02587 0.01243 -0.1560 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.