Date: 7.5.2001 PARTICIPANT INFORMATION ----------------------- Name: Mark Rakowitz, Bernhard Eisfeld, Hans Bleecke, Jens Fassbender Email: mark.rakowitz.@dlr.de Phone: +49 (531) 295-2415 Address: Institute of Design Aerodynamics Address: Lilienthalplatz 7 Address: D-38108 Braunschweig Address: Germany Address: Address: SOLVER INFORMATION -------------------- Method Name: FLOWer Basic Algorithm: 2nd order, central discretization + artificial dissipation Turbulence Model: LEA k-omega Miscellaneous: Cell-centered, multigrid, turbulence equations implicit 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: MegaCads Grid Type: Body-fitted structured C-O-H topology Zones: 7 Field Nodes: 3689127 Field Cells: 3507200 Boundary Nodes: 57806 Boundary Faces: 56320 BL 1st-Cell Size: 0.0204 mm BL Max-Growth Rate: 1.4 BL Cells: 20 Miscellaneous: 32 cells in BL-block, about 20 cells in BL SOLUTION INFORMATION -------------------- Computer Platform: SX5 # Processors: 1 Operating System: SUPER-UX 10.1 revision 1 Compiler: sxf90 revision 205 crosscompiler Run Time CPU: case1: 38651s case2: 28200s Run Time Wall-Clock: case1: 39312s case2: 29600s Memory Requirements: 3.14 GB Miscellaneous: Time for case2 averaged CASE 1 DATA ON PROVIDED GRID (REQUIRED) --------------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -0.180 0.500 0.02760 0.01795 0.00965 0.1546 CASE 2 DRAG POLAR DATA (REQUIRED) --------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -3.0 0.123 0.02400 0.01020 0.01380 0.1492 0.75 -2.0 0.238 0.02514 0.01138 0.01376 0.1463 0.75 -1.0 0.352 0.02768 0.01399 0.01369 0.1423 0.75 0.0 0.466 0.03191 0.01832 0.01359 0.1362 0.75 1.0 0.589 0.03933 0.02590 0.01343 0.1308 0.75 2.0 0.702 0.05151 0.03837 0.01314 0.1229 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: 7.5.2001 PARTICIPANT INFORMATION ----------------------- Name: Mark Rakowitz, Bernhard Eisfeld, Hans Bleecke, Jens Fassbender Email: mark.rakowitz.@dlr.de Phone: +49 (531) 295-2415 Address: Institute of Design Aerodynamics Address: Lilienthalplatz 7 Address: D-38108 Braunschweig Address: Germany Address: Address: SOLVER INFORMATION -------------------- Method Name: FLOWer Basic Algorithm: 2nd order, central discretization + artificial dissipation Turbulence Model: LEA k-omega Miscellaneous: Cell-centered, multigrid, turbulence equations implicit 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: MegaCads Grid Type: Body-fitted structured C-O-H topology Zones: 7 Field Nodes: 3689127 Field Cells: 3507200 Boundary Nodes: 57806 Boundary Faces: 56320 BL 1st-Cell Size: 0.001 mm BL Max-Growth Rate: 1.4 BL Cells: 20 Miscellaneous: 32 cells in BL-block, about 20 cells in BL SOLUTION INFORMATION -------------------- Computer Platform: SX5 # Processors: 1 Operating System: SUPER-UX 10.1 revision 1 Compiler: sxf90 revision 205 crosscompiler Run Time CPU: case1: 38651s case2: 28200s Run Time Wall-Clock: case1: 39312s case2: 29600s Memory Requirements: 3.14 GB Miscellaneous: Time for case2 averaged CASE 1 DATA ON PROVIDED GRID (REQUIRED) --------------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -0.180 0.500 0.02760 0.01795 0.00965 -0.1546 CASE 2 DRAG POLAR DATA (REQUIRED) --------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -3.0 0.123 0.02400 0.01020 0.01380 -0.1492 0.75 -2.0 0.238 0.02514 0.01138 0.01376 -0.1463 0.75 -1.0 0.352 0.02768 0.01399 0.01369 -0.1423 0.75 0.0 0.466 0.03191 0.01832 0.01359 -0.1362 0.75 1.0 0.589 0.03933 0.02590 0.01343 -0.1308 0.75 2.0 0.702 0.05151 0.03837 0.01314 -0.1229 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: 7.5.2001 PARTICIPANT INFORMATION ----------------------- Name: Mark Rakowitz, Bernhard Eisfeld, Hans Bleecke, Jens Fassbender Email: mark.rakowitz.@dlr.de Phone: +49 (531) 295-2415 Address: Institute of Design Aerodynamics Address: Lilienthalplatz 7 Address: D-38108 Braunschweig Address: Germany Address: Address: SOLVER INFORMATION -------------------- Method Name: FLOWer Basic Algorithm: 2nd order, central discretization + artificial dissipation Turbulence Model: Wilcox k-omega Miscellaneous: Cell-centered, multigrid, turbulence equations implicit 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: MegaCads Grid Type: Body-fitted structured C-O-H topology Zones: 7 Field Nodes: 3689127 Field Cells: 3507200 Boundary Nodes: 57806 Boundary Faces: 56320 BL 1st-Cell Size: 0.0204 mm BL Max-Growth Rate: 1.4 BL Cells: 20 Miscellaneous: 32 cells in BL-block, about 20 cells in BL SOLUTION INFORMATION -------------------- Computer Platform: SX5 # Processors: 1 Operating System: SUPER-UX 10.1 revision 1 Compiler: sxf90 revision 205 crosscompiler Run Time CPU: case1: 33999s case2: 21200s case3: 30300s case4: 30300s Run Time Wall-Clock: case1: 34794s case2: 21400s case3: 33000s case4: 33000s Memory Requirements: 3.09 GB Miscellaneous: Times for cases2-4 averaged CASE 1 DATA ON PROVIDED GRID (REQUIRED) --------------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -0.296 0.500 0.02762 0.01778 0.00985 0.1602 CASE 2 DRAG POLAR DATA (REQUIRED) --------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -3.0 0.154 0.02429 0.01010 0.01419 0.1597 0.75 -2.0 0.271 0.02572 0.01157 0.01415 0.1568 0.75 -1.0 0.386 0.02857 0.01449 0.01408 0.1528 0.75 0.0 0.502 0.03317 0.01921 0.01396 0.1464 0.75 1.0 0.622 0.04094 0.02718 0.01376 0.1388 0.75 2.0 0.734 0.05350 0.04003 0.01347 0.1308 CASE 3 DRAG RISE DATA (OPTIONAL) -------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.50 0.769 0.500 0.03171 0.01661 0.01510 0.1181 0.60 0.537 0.500 0.03168 0.01701 0.01467 0.1262 0.70 0.226 0.500 0.03237 0.01817 0.01420 0.1373 0.75 -0.019 0.500 0.03306 0.01910 0.01396 0.1465 0.76 -0.084 0.500 0.03321 0.01930 0.01391 0.1492 0.77 -0.158 0.500 0.03340 0.01954 0.01386 0.1526 0.78 -0.240 0.500 0.03374 0.01995 0.01380 0.1571 0.80 -0.296 0.500 0.03648 0.02289 0.01359 0.1643 CASE 4 ADDITIONAL DRAG RISE DATA (OPTIONAL) ------------------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.50 -0.314 0.400 0.02809 0.01290 0.01519 0.1269 0.60 -0.487 0.400 0.02804 0.01328 0.01476 0.1341 0.70 -0.720 0.400 0.02846 0.01414 0.01431 0.1444 0.75 -0.882 0.400 0.02901 0.01494 0.01407 0.1521 0.76 -0.923 0.400 0.02916 0.01515 0.01402 0.1542 0.77 -0.969 0.400 0.02935 0.01539 0.01396 0.1567 0.78 -1.013 0.400 0.02967 0.01578 0.01390 0.1595 0.80 -1.079 0.400 0.03097 0.01723 0.01374 0.1655 MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.50 1.868 0.600 0.03638 0.02140 0.01498 0.1081 0.60 1.581 0.600 0.03651 0.02198 0.01452 0.1167 0.70 1.206 0.600 0.03837 0.02433 0.01404 0.1267 0.75 0.820 0.600 0.03919 0.02539 0.01380 0.1400 0.76 0.720 0.600 0.03948 0.02573 0.01375 0.1447 0.77 0.620 0.600 0.04002 0.02633 0.01369 0.1503 0.78 0.552 0.600 0.04123 0.02762 0.01361 0.1553 0.80 0.768 0.600 0.04806 0.03478 0.01328 0.1513 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: 7.5.2001 PARTICIPANT INFORMATION ----------------------- Name: Mark Rakowitz, Bernhard Eisfeld, Hans Bleecke, Jens Fassbender Email: mark.rakowitz.@dlr.de Phone: +49 (531) 295-2415 Address: Institute of Design Aerodynamics Address: Lilienthalplatz 7 Address: D-38108 Braunschweig Address: Germany Address: Address: SOLVER INFORMATION -------------------- Method Name: FLOWer Basic Algorithm: 2nd order, central discretization + artificial dissipation Turbulence Model: Wilcox k-omega Miscellaneous: Cell-centered, multigrid, turbulence equations implicit 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: MegaCads Grid Type: Body-fitted structured C-O-H topology Zones: 7 Field Nodes: 3689127 Field Cells: 3507200 Boundary Nodes: 57806 Boundary Faces: 56320 BL 1st-Cell Size: 0.001 mm BL Max-Growth Rate: 1.4 BL Cells: 20 Miscellaneous: 32 cells in BL-block, about 20 cells in BL SOLUTION INFORMATION -------------------- Computer Platform: SX5 # Processors: 1 Operating System: SUPER-UX 10.1 revision 1 Compiler: sxf90 revision 205 crosscompiler Run Time CPU: case1: 33999s case2: 21200s case3: 30300s case4: 30300s Run Time Wall-Clock: case1: 34794s case2: 21400s case3: 33000s case4: 33000s Memory Requirements: 3.09 GB Miscellaneous: Times for cases2-4 averaged CASE 1 DATA ON PROVIDED GRID (REQUIRED) --------------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -0.296 0.500 0.02762 0.01778 0.00985 -0.1602 CASE 2 DRAG POLAR DATA (REQUIRED) --------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -3.0 0.154 0.02429 0.01010 0.01419 -0.1597 0.75 -2.0 0.271 0.02572 0.01157 0.01415 -0.1568 0.75 -1.0 0.386 0.02857 0.01449 0.01408 -0.1528 0.75 0.0 0.502 0.03317 0.01921 0.01396 -0.1464 0.75 1.0 0.622 0.04094 0.02718 0.01376 -0.1388 0.75 2.0 0.734 0.05350 0.04003 0.01347 -0.1308 CASE 3 DRAG RISE DATA (OPTIONAL) -------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.50 0.769 0.500 0.03171 0.01661 0.01510 -0.1181 0.60 0.537 0.500 0.03168 0.01701 0.01467 -0.1262 0.70 0.226 0.500 0.03237 0.01817 0.01420 -0.1373 0.75 -0.019 0.500 0.03306 0.01910 0.01396 -0.1465 0.76 -0.084 0.500 0.03321 0.01930 0.01391 -0.1492 0.77 -0.158 0.500 0.03340 0.01954 0.01386 -0.1526 0.78 -0.240 0.500 0.03374 0.01995 0.01380 -0.1571 0.80 -0.296 0.500 0.03648 0.02289 0.01359 -0.1643 CASE 4 ADDITIONAL DRAG RISE DATA (OPTIONAL) ------------------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.50 -0.314 0.400 0.02809 0.01290 0.01519 -0.1269 0.60 -0.487 0.400 0.02804 0.01328 0.01476 -0.1341 0.70 -0.720 0.400 0.02846 0.01414 0.01431 -0.1444 0.75 -0.882 0.400 0.02901 0.01494 0.01407 -0.1521 0.76 -0.923 0.400 0.02916 0.01515 0.01402 -0.1542 0.77 -0.969 0.400 0.02935 0.01539 0.01396 -0.1567 0.78 -1.013 0.400 0.02967 0.01578 0.01390 -0.1595 0.80 -1.079 0.400 0.03097 0.01723 0.01374 -0.1655 MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.50 1.868 0.600 0.03638 0.02140 0.01498 -0.1081 0.60 1.581 0.600 0.03651 0.02198 0.01452 -0.1167 0.70 1.206 0.600 0.03837 0.02433 0.01404 -0.1267 0.75 0.820 0.600 0.03919 0.02539 0.01380 -0.1400 0.76 0.720 0.600 0.03948 0.02573 0.01375 -0.1447 0.77 0.620 0.600 0.04002 0.02633 0.01369 -0.1503 0.78 0.552 0.600 0.04123 0.02762 0.01361 -0.1553 0.80 0.768 0.600 0.04806 0.03478 0.01328 -0.1513 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: 7.5.2001 PARTICIPANT INFORMATION ----------------------- Name: Mark Rakowitz, Bernhard Eisfeld, Hans Bleecke, Jens Fassbender Email: mark.rakowitz.@dlr.de Phone: +49 (531) 295-2415 Address: Institute of Design Aerodynamics Address: Lilienthalplatz 7 Address: D-38108 Braunschweig Address: Germany Address: Address: SOLVER INFORMATION -------------------- Method Name: FLOWer Basic Algorithm: 2nd order, central discretization + artificial dissipation Turbulence Model: Wilcox k-omega Miscellaneous: Cell-centered, singlegrid, turbulence equations implicit 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: MegaCads Grid Type: Body-fitted structured C-O-H topology Zones: 7 Field Nodes: 5223598 Field Cells: 4993650 Boundary Nodes: 72951 Boundary Faces: 71280 BL 1st-Cell Size: 0.0181 mm BL Max-Growth Rate: 1.4 BL Cells: 23 Miscellaneous: 36 cells in BL-block, about 20 cells in BL SOLUTION INFORMATION -------------------- Computer Platform: SX5 # Processors: 1 Operating System: SUPER-UX 10.1 revision 1 Compiler: sxf90 revision 205 crosscompiler Run Time CPU: case2: 167000s Run Time Wall-Clock: case2: 170000s Memory Requirements: 3.84 GB Miscellaneous: Time for cases2 averaged CASE 2 DRAG POLAR DATA (REQUIRED) --------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -3.0 0.161 0.02258 0.00892 0.01366 0.1642 0.75 -2.0 0.278 0.02415 0.01053 0.01362 0.1613 0.75 -1.0 0.395 0.02711 0.01356 0.01355 0.1577 0.75 0.0 0.514 0.03178 0.01836 0.01343 0.1518 0.75 1.0 0.637 0.03980 0.02657 0.01323 0.1453 0.75 2.0 0.750 0.05280 0.03986 0.01294 0.1370 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: 7.5.2001 PARTICIPANT INFORMATION ----------------------- Name: Mark Rakowitz, Bernhard Eisfeld, Hans Bleecke, Jens Fassbender Email: mark.rakowitz.@dlr.de Phone: +49 (531) 295-2415 Address: Institute of Design Aerodynamics Address: Lilienthalplatz 7 Address: D-38108 Braunschweig Address: Germany Address: Address: SOLVER INFORMATION -------------------- Method Name: FLOWer Basic Algorithm: 2nd order, central discretization + artificial dissipation Turbulence Model: Wilcox k-omega Miscellaneous: Cell-centered, singlegrid, turbulence equations implicit 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: MegaCads Grid Type: Body-fitted structured C-O-H topology Zones: 7 Field Nodes: 5223598 Field Cells: 4993650 Boundary Nodes: 72951 Boundary Faces: 71280 BL 1st-Cell Size: 0.00088 mm BL Max-Growth Rate: 1.4 BL Cells: 23 Miscellaneous: 36 cells in BL-block, about 20 cells in BL SOLUTION INFORMATION -------------------- Computer Platform: SX5 # Processors: 1 Operating System: SUPER-UX 10.1 revision 1 Compiler: sxf90 revision 205 crosscompiler Run Time CPU: case2: 167000s Run Time Wall-Clock: case2: 170000s Memory Requirements: 3.84 GB Miscellaneous: Time for cases2 averaged CASE 2 DRAG POLAR DATA (REQUIRED) --------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -3.0 0.161 0.02258 0.00892 0.01366 -0.1642 0.75 -2.0 0.278 0.02415 0.01053 0.01362 -0.1613 0.75 -1.0 0.395 0.02711 0.01356 0.01355 -0.1577 0.75 0.0 0.514 0.03178 0.01836 0.01343 -0.1518 0.75 1.0 0.637 0.03980 0.02657 0.01323 -0.1453 0.75 2.0 0.750 0.05280 0.03986 0.01294 -0.1370 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.