Date: 5/7/01 PARTICIPANT INFORMATION ----------------------- Name: Christopher L. Rumsey Email: c.l.rumsey@larc.nasa.gov Phone: (757) 864-2165 Address: NASA LaRC Address: MS 128 Address: Hampton, VA 23681 Address: Address: Address: SOLVER INFORMATION -------------------- Method Name: CFL3D Version 6.0 Basic Algorithm: upwind finite-volume FDS Turbulence Model: EASM (k-omega) Miscellaneous: Turb model described in AIAA 2000-4323 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: SGI Origin 2000, 32 R10000 250Mhz processors, 4Mb level 2 cache # Processors: 4 + host Operating System: 6.5 6.5.11m Compiler: MIPSpro Compilers: Version 7.3.1.2m Run Time CPU: Run Time Wall-Clock: 40 hours for 800 cycles typical (depends on machine load) Memory Requirements: 2.17 gigabytes (double precision) Miscellaneous: CASE 1 DATA ON PROVIDED GRID (REQUIRED) --------------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -0.345 0.500 0.02953 0.01764 0.01189 -0.1644 CASE 2 DRAG POLAR DATA (REQUIRED) --------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -3.0 0.179 0.02088 0.00888 0.01200 -0.1711 0.75 -2.0 0.301 0.02295 0.01096 0.01199 -0.1706 0.75 -1.0 0.422 0.02642 0.01448 0.01194 -0.1680 0.75 0.0 0.542 0.03152 0.01967 0.01185 -0.1619 0.75 1.0 0.668 0.03992 0.02824 0.01168 -0.1559 0.75 2.0 0.771 0.05280 0.04138 0.01142 -0.1422 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: 5/7/01 PARTICIPANT INFORMATION ----------------------- Name: Christopher L. Rumsey Email: c.l.rumsey@larc.nasa.gov Phone: (757) 864-2165 Address: NASA LaRC Address: MS 128 Address: Hampton, VA 23681 Address: Address: Address: SOLVER INFORMATION -------------------- Method Name: CFL3D Version 6.0 Basic Algorithm: upwind finite-volume FDS Turbulence Model: Spalart-Allmaras, version Ia Miscellaneous: Turb model described in La Recherche Aerospatiale 1, 1994 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: SGI Origin 2000, 32 R10000 250Mhz processors, 4Mb level 2 cache # Processors: 4 + host Operating System: 6.5 6.5.11m Compiler: MIPSpro Compilers: Version 7.3.1.2m Run Time CPU: Run Time Wall-Clock: 28 hours for 800 cycles typical (depends on machine load) Memory Requirements: 2.17 gigabytes (double precision) Miscellaneous: CASE 1 DATA ON PROVIDED GRID (REQUIRED) --------------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -0.345 0.500 0.03145 0.01746 0.01399 -0.1656 CASE 2 DRAG POLAR DATA (REQUIRED) --------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -3.0 0.176 0.02270 0.00857 0.01414 -0.1713 0.75 -2.0 0.299 0.02481 0.01069 0.01412 -0.1708 0.75 -1.0 0.420 0.02830 0.01424 0.01406 -0.1685 0.75 0.0 0.542 0.03346 0.01953 0.01393 -0.1633 0.75 1.0 0.663 0.04168 0.02802 0.01366 -0.1550 0.75 2.0 0.760 0.05417 0.04090 0.01327 -0.1385 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: 5/7/01 PARTICIPANT INFORMATION ----------------------- Name: Christopher L. Rumsey Email: c.l.rumsey@larc.nasa.gov Phone: (757) 864-2165 Address: NASA LaRC Address: MS 128 Address: Hampton, VA 23681 Address: Address: Address: SOLVER INFORMATION -------------------- Method Name: CFL3D Version 6.0 Basic Algorithm: upwind finite-volume FDS Turbulence Model: Spalart-Allmaras with fv3 (unpublished) Miscellaneous: This version of S-A is in many codes (e.g. INS3D, OVERFLOW) 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: SGI Origin 2000, 32 R10000 250Mhz processors, 4Mb level 2 cache # Processors: 4 + host Operating System: 6.5 6.5.11m Compiler: MIPSpro Compilers: Version 7.3.1.2m Run Time CPU: Run Time Wall-Clock: 28 hours for 800 cycles typical (depends on machine load) Memory Requirements: 2.17 gigabytes (double precision) Miscellaneous: Part of parametric study - all required cases not done CASE 1 DATA ON PROVIDED GRID (REQUIRED) --------------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 ?.??? 0.50? ?.????? ?.????? ?.????? ?.???? CASE 2 DRAG POLAR DATA (REQUIRED) --------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 0.0 0.552 0.03332 0.01961 0.01371 -0.1687 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: 5/7/01 PARTICIPANT INFORMATION ----------------------- Name: Christopher L. Rumsey Email: c.l.rumsey@larc.nasa.gov Phone: (757) 864-2165 Address: NASA LaRC Address: MS 128 Address: Hampton, VA 23681 Address: Address: Address: SOLVER INFORMATION -------------------- Method Name: CFL3D Version 6.0 Basic Algorithm: upwind finite-volume FDS Turbulence Model: Spalart-Allmaras, version Ia Miscellaneous: Transition set to match "fully turb" (free) transition of EASM 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: SGI Origin 2000, 32 R10000 250Mhz processors, 4Mb level 2 cache # Processors: 4 + host Operating System: 6.5 6.5.11m Compiler: MIPSpro Compilers: Version 7.3.1.2m Run Time CPU: Run Time Wall-Clock: 28 hours for 800 cycles typical (depends on machine load) Memory Requirements: 2.17 gigabytes (double precision) Miscellaneous: Part of parametric study - all required cases not done CASE 1 DATA ON PROVIDED GRID (REQUIRED) --------------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -0.356 0.500 0.03136 0.01741 0.01395 -0.1664 CASE 2 DRAG POLAR DATA (REQUIRED) --------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -3.0 ?.??? ?.????? ?.????? ?.????? ?.???? 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: 5/7/01 PARTICIPANT INFORMATION ----------------------- Name: Christopher L. Rumsey Email: c.l.rumsey@larc.nasa.gov Phone: (757) 864-2165 Address: NASA LaRC Address: MS 128 Address: Hampton, VA 23681 Address: Address: Address: SOLVER INFORMATION -------------------- Method Name: CFL3D Version 6.0 Basic Algorithm: upwind finite-volume FDS Turbulence Model: Menter's SST k-omega Miscellaneous: Turb model described in AIAA Journal 32(8), 1994 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: SGI Origin 2000, 32 R10000 250Mhz processors, 4Mb level 2 cache # Processors: 4 + host Operating System: 6.5 6.5.11m Compiler: MIPSpro Compilers: Version 7.3.1.2m Run Time CPU: Run Time Wall-Clock: 30 hours for 800 cycles typical (depends on machine load) Memory Requirements: 2.17 gigabytes (double precision) Miscellaneous: Part of parametric study - all required cases not done CASE 1 DATA ON PROVIDED GRID (REQUIRED) --------------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -0.345 0.500 0.02964 0.01746 0.01217 -0.1650 CASE 2 DRAG POLAR DATA (REQUIRED) --------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -1.0 0.421 0.02651 0.01427 0.01223 -0.1682 0.75 0.0 0.542 0.03164 0.01952 0.01212 -0.1629 0.75 1.0 0.666 0.03997 0.02807 0.01190 -0.1559 0.75 2.0 0.759 0.05245 0.04089 0.01156 -0.1374 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: 5/7/01 PARTICIPANT INFORMATION ----------------------- Name: Christopher L. Rumsey Email: c.l.rumsey@larc.nasa.gov Phone: (757) 864-2165 Address: NASA LaRC Address: MS 128 Address: Hampton, VA 23681 Address: Address: Address: SOLVER INFORMATION -------------------- Method Name: CFL3D Version 6.0 Basic Algorithm: upwind finite-volume FDS Turbulence Model: Spalart-Allmaras version Ia Miscellaneous: 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: SGI Origin 2000, 32 R10000 250Mhz processors, 4Mb level 2 cache # Processors: 3 + host Operating System: 6.5 6.5.11m Compiler: MIPSpro Compilers: Version 7.3.1.2m Run Time CPU: Run Time Wall-Clock: 120 hours for 2200 cycles typical (depends on machine load) Memory Requirements: 2.54 gigabytes (double precision) Miscellaneous: Part of parametric study - all required cases not done CASE 1 DATA ON PROVIDED GRID (REQUIRED) --------------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 ?.??? 0.50? ?.????? ?.????? ?.????? ?.???? CASE 2 DRAG POLAR DATA (REQUIRED) --------------------------------- MACH ALPHA CL_TOT CD_TOT CD_PR CD_SF CM_TOT 0.75 -1.0 0.418 0.02792 0.01402 0.01390 -0.1639 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.