Date: 06 May, 2001 PARTICIPANT INFORMATION ----------------------- Name: John C. Vassberg Email: john.c.vassberg@boeing.com Phone: 562.593-9604 Address: The Boeing Company Address: Phantom Works Address: Aerodynamics Address: Mail Code: C078-0421 Address: 2401 E. Wardlow Road Address: Long Beach, CA 90807-5309 SOLVER INFORMATION -------------------- Method Name: OVERFLOW_1.8M Basic Algorithm: Over-Set Grid Turbulence Model: Spalart-Allmaras Miscellaneous: Parallel Processing under MPI CASE 1 PROVIDED GRID USED Mark one line with an X -------------------- Multi-block: Overset: X 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: Hewlett-Packard C3610 # Processors: 6 Operating System: HP-UX 10.20 Compiler: mpif90 +O3 +U77 +Odataprefetch +Ovectorize -Wl,+FPZOD Run Time CPU: 240,000 sec / 3000 iter = 80.00 sec/iter Run Time Wall-Clock: 46,977 sec / 3000 iter = 15.66 sec/iter Memory Requirements: 1.8 GB = 480 Bytes / Grid Point Miscellaneous: 150_C/150_I/3000_F Iterations, -DD_PRECISION -DMPI CASE 1 DATA ON PROVIDED GRID (REQUIRED) --------------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT .75 -.257 .50000 .02958 .01575 .01383 -.16308 CASE 2 DRAG POLAR DATA (REQUIRED) --------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT .75 -3.000 .16628 .02125 .00725 .01400 -.17181 .75 -2.000 .28749 .02315 .00917 .01398 -.16989 .75 -1.000 .40864 .02633 .01241 .01392 -.16683 .75 .000 .53174 .03095 .01718 .01377 -.16125 .75 .500 .59596 .03434 .02069 .01365 -.15793 .75 1.000 .66373 .03904 .02557 .01347 -.15566 .75 1.500 .72021 .04489 .03163 .01327 -.15062 .75 2.000 .76821 .05189 .03884 .01305 -.14267 CASE 3 DRAG RISE DATA (OPTIONAL) -------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT .50 .496 .50000 .02911 .01422 .01489 -.13411 .60 .258 .50000 .02899 .01446 .01453 -.14290 .70 -.042 .50000 .02927 .01517 .01409 -.15424 .75 -.257 .50000 .02958 .01575 .01383 -.16308 .76 -.309 .50000 .02970 .01594 .01376 -.16542 .77 -.358 .50000 .02990 .01620 .01369 -.16794 .78 -.410 .50000 .03020 .01657 .01361 -.17092 .79 -.457 .50000 .03080 .01727 .01353 -.17465 .80 -.434 .50000 .03241 .01901 .01339 -.17565 .82 .074 .50000 .04021 .02725 .01296 -.15795 CASE 4 ADDITIONAL DRAG RISE DATA (OPTIONAL) ------------------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT .50 -.528 .40000 .02577 .01084 .01494 -.14174 .60 -.716 .40000 .02562 .01103 .01459 -.14945 .70 -.934 .40000 .02577 .01159 .01418 -.15981 .75 -1.071 .40000 .02607 .01214 .01392 -.16705 .76 -1.102 .40000 .02617 .01230 .01387 -.16892 .77 -1.133 .40000 .02633 .01253 .01380 -.17095 .78 -1.158 .40000 .02665 .01293 .01372 -.17310 .79 -1.165 .40000 .02720 .01357 .01363 -.17479 .80 -1.163 .40000 .02791 .01437 .01353 -.17612 .82 -.987 .40000 .03127 .01804 .01325 -.17189 MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT .50 1.529 .60000 .03326 .01845 .01481 -.12584 .60 1.245 .60000 .03327 .01884 .01442 -.13524 .70 .866 .60000 .03416 .02025 .01390 -.14630 .75 .530 .60000 .03461 .02097 .01364 -.15779 .76 .455 .60000 .03477 .02119 .01357 -.16097 .77 .386 .60000 .03514 .02163 .01350 -.16516 .78 .325 .60000 .03622 .02283 .01340 -.16931 .79 .372 .60000 .03869 .02544 .01325 -.16906 .80 .629 .60000 .04348 .03045 .01303 -.15941 .82 1.439 .60000 .05681 .04430 .01250 -.13099 MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT .50 -1.567 .30000 .02322 .00824 .01498 -.14939 .60 -1.688 .30000 .02306 .00842 .01464 -.15551 .70 -1.822 .30000 .02316 .00893 .01423 -.16387 .75 -1.897 .30000 .02343 .00945 .01397 -.16957 .76 -1.912 .30000 .02350 .00959 .01392 -.17100 .77 -1.927 .30000 .02362 .00977 .01385 -.17250 .78 -1.940 .30000 .02381 .01002 .01379 -.17424 .79 -1.944 .30000 .02416 .01046 .01370 -.17583 .80 -1.927 .30000 .02477 .01116 .01360 -.17697 .82 -1.784 .30000 .02705 .01371 .01336 -.17428 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.