Date: 3 May 2001 PARTICIPANT INFORMATION ----------------------- Name: George Waller Email: gwaller@dehavilland.ca Phone: 416 373 7751 Address: 123 Garratt Blvd. N46-34 Address: Downsview Address: Toronto Address: Ontario Address: Canada Address: M3K 1Y5 SOLVER INFORMATION -------------------- Method Name: MGAERO Basic Algorithm: Finite-difference, multi-grid Euler code Turbulence Model: Integral boundary layer Miscellaneous: Cartesian grids CASE 1 PROVIDED GRID USED Mark one line with an X -------------------- Multi-block: Overset: Unstructured node: Unstructured cell: Could not use: X GRID INFORMATION FOR CASES 2-4 Leave blank if you used the Case 1 provided grid -------------------- Grid-Generator Name: CATPAN Grid Type: Cartesian Zones: 31 Field Nodes: 2518066 Field Cells: Boundary Nodes: Boundary Faces: BL 1st-Cell Size: BL Max-Growth Rate: BL Cells: Miscellaneous: Euler grid SOLUTION INFORMATION -------------------- Computer Platform: SGI Origin 200 # Processors: 1 Operating System: Unix Compiler: F90 Run Time CPU: 15.58 hours Run Time Wall-Clock: 15.58 hours Memory Requirements: 540Mbytes Miscellaneous: CASE 1 DATA ON PROVIDED GRID (REQUIRED) --------------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -1.00 0.498 0.02683 0.01211 0.01472 -0.2276 CASE 2 DRAG POLAR DATA (REQUIRED) --------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -3.0 0.275 0.01997 0.00552 0.01445 -0.2424 0.75 -2.0 0.377 0.02245 0.00795 0.01450 -0.2318 0.75 -1.0 0.498 0.02683 0.01211 0.01472 -0.2276 0.75 0.0 0.629 0.03269 0.01783 0.01486 -0.2255 0.75 1.0 0.777 0.04450 0.02935 0.01516 -0.2389 0.75 2.0 0.916 0.06514 0.04966 0.01548 0.9396 CASE 3 DRAG RISE DATA (OPTIONAL) -------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.50 -0.375 0.500 0.02683 0.01240 0.01443 -0.1304 0.60 -0.535 0.500 0.02670 0.01228 0.01443 -0.1923 0.70 -0.859 0.500 0.02659 0.01206 0.01453 -0.2189 0.75 -1.000 0.500 0.02668 0.01203 0.01465 -0.2196 0.76 -1.047 0.500 0.02725 0.01259 0.01467 -0.2271 0.77 -1.141 0.500 0.02785 0.01323 0.01462 -0.2296 0.78 -1.281 0.500 0.02821 0.01350 0.01471 -0.2413 0.80 -1.656 0.500 0.03090 0.01619 0.01471 -0.2714 CASE 4 ADDITIONAL DRAG RISE DATA (OPTIONAL) ------------------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.50 -0.938 0.400 0.02275 0.00841 0.01434 -0.1854 0.60 -0.844 0.400 0.02246 0.00821 0.01425 -0.1854 0.70 -1.188 0.400 0.02215 0.00784 0.01431 -0.2189 0.75 -1.812 0.400 0.02207 0.00767 0.01440 -0.2387 0.76 -1.750 0.400 0.02213 0.00771 0.01442 -0.2512 0.77 -1.640 0.400 0.02249 0.00802 0.01447 -0.2345 0.78 -1.750 0.400 0.02244 0.00796 0.01448 -0.2533 0.80 -1.875 0.400 0.02354 0.00906 0.01448 -0.2607 MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.50 0.775 0.600 0.03034 0.01600 0.01434 -0.1837 0.60 0.494 0.600 0.02997 0.01552 0.01445 -0.1966 0.70 0.025 0.600 0.02980 0.01523 0.01457 -0.2081 0.75 -0.225 0.600 0.02966 0.01500 0.01466 -0.2318 0.76 -0.163 0.600 0.02951 0.01485 0.01466 -0.2259 0.77 -0.413 0.600 0.03010 0.01541 0.01469 -0.2437 0.78 -0.412 0.600 0.03100 0.01634 0.01466 -0.2485 0.80 -0.850 0.600 0.03280 0.01810 0.01470 -0.2624 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.