Date: 5/7/2001 PARTICIPANT INFORMATION ----------------------- Name: Thomas Scheidegger Email: tes@fluent.com Phone: 603-643-2600 x236 Name: Greg Stuckert Email: gks@fluent.com Phone: 603-643-2600 x243 Name: Sutikno Wirogo (non-participant) Email: sw@fluent.com Phone: 603-643-2600 x247 Address: 10 Cavendish Court, Centerra Resource Park Address: Lebanon, NH 03766-1442 SOLVER INFORMATION -------------------- Method Name: Fluent5 Basic Algorithm: unstructured finite-volume, SIMPLE, second-order upwind Turbulence Model: realizable k-epsilon Miscellaneous: CASE 1 PROVIDED GRID USED Mark one line with an X -------------------- Multi-block: X 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: HP J6000, 552Mhz PA8600 # Processors: 2 Operating System: HPUX11.0 Compiler: HP92453 A.11.01.00 Run Time CPU: 288 CPU-hours Run Time Wall-Clock: 144 hours Memory Requirements: 5.6 GB RAM Miscellaneous: dual processor machine with 8GB RAM CASE 1 DATA ON PROVIDED GRID (REQUIRED) --------------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 1.223 0.502 0.04998 0.03263 0.01734 0.0481 CASE 2 DRAG POLAR DATA (REQUIRED) --------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -3.0 0.074 0.03404 0.01615 0.01789 -0.1252 0.75 -2.0 0.185 0.03526 0.01735 0.01791 -0.1227 0.75 -1.0 0.293 0.03798 0.02012 0.01786 -0.1180 0.75 0.0 0.394 0.04227 0.02455 0.01772 -0.1106 0.75 1.0 0.483 0.04832 0.03089 0.01742 -0.0990 0.75 2.0 0.552 0.05641 0.03945 0.01695 -0.0819 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.