Date: PARTICIPANT INFORMATION ----------------------- Name: Peter Eliasson, Shia-Hui Peng Email: enp@foi.se (Peter Eliasson), peng@foi.se (Shia-Hui Peng) Phone: +46-8-5550 4371 (Peter Eliasson),+46-8-5550 4325 (Shia-Hui Peng) Address: Computational Aerodynamics Aeronautics Division (FFA) Swedish Defence Research Agency (FOI) S-171 92 Stockholm Sweden SOLVER INFORMATION -------------------- Method Name: EDGE, a unstructured edge-based solver Basic Algorithm: Unstructured Mixed Element Turbulence Model: Two-equation k-omega + Algebraic stress model Residual: L2 Miscellaneous: Note that all results are converged so that oscillations in forces and moments are < 0.1% of its converged value Note also: fully turbulence is assumed. GRID INFORMATION -------------------- Grid-Generator Name: Generated by DLR (using Centaur software from CentaurSoft) Grid Type: Hybrid COARSE GRID SIZE WB WBNP ----------------------------------------- Zones: Field Nodes: 2390716 3682535 Field Cells: Boundary Nodes: Boundary Faces: BL 1st-Cell Size: BL Max-Growth Rate: BL Cells: Miscellaneous: MEDIUM GRID SIZE WB WBNP ----------------------------------------- Zones: Field Nodes: 3159195 4787893 Field Cells: Boundary Nodes: Boundary Faces: BL 1st-Cell Size: BL Max-Growth Rate: BL Cells: Miscellaneous: FINE GRID SIZE WB WBNP ----------------------------------------- Zones: Field Nodes: 4095096 6381216 Field Cells: Boundary Nodes: Boundary Faces: BL 1st-Cell Size: BL Max-Growth Rate: BL Cells: Miscellaneous: SOLUTION INFORMATION -------------------- Computer Platform: Clustered Compact machine # Processors: 4-10 Operating System: Compiler: Run Time CPU: Run Time Wall-Clock: Memory Requirements: Miscellaneous: CASE 1 SINGLE-POINT GRID CONVERGENCE STUDY (REQUIRED) --------------------------------------- WING/BODY GRID_SIZE MACH ALPHA CL_TOT (min, max) CD_TOT (min, max) CD_PR CD_SF CM_TOT (min, max) RESID_DROP WB_C 0.75 0.0 4.9466E-01 (steady) 2.6916E-02 (steady) 1.5793E-02 1.1123E-02 -1.4028E-01 (steady) -6.0 WB_M 0.75 0.0 4.9355E-01 (steady) 2.6232E-02 (steady) 1.5386E-02 1.0845E-02 -1.3948E-01 (steady) -5.7 WB_F 0.75 0.0 4.9893E-01 (steady) 2.7280E-02 (steady) 1.5706E-02 1.1574E-02 -1.4918E-01 (steady) -2.7 WING/BODY/NACELLE/PYLON GRID_SIZE MACH ALPHA CL_TOT (min, max) CD_TOT (min, max) CD_PR CD_SF CM_TOT (min, max) RESID_DROP WBNP_C 0.75 0.5 4.9255E-01 (steady) 3.1115E-02 (steady) 1.7870E-02 1.3246E-02 -1.3851E-01 (steady) -6.2 WBNP_M 0.75 0.5 4.9393E-01 (steady) 3.0060E-02 (steady) 1.7081E-02 1.2978E-02 -1.3977E-01 (steady) -5.8 WBNP_F 0.75 0.5 4.9318E-01 (steady) 2.9702E-02 (steady) 1.6700E-02 1.3002E-02 -1.3940E-01 (steady) -5.5 SEPARATION BUBBLE GEOMETRY - WING/BODY - FINE GRID FS_BUB BL_BUB WL_BUB 1.9704E-01 -9.4853E-02 8.9064E-03 FS_EYE_W BL_EYE_W WL_EYE_W 2.3612E-01 -7.7474E-02 -9.1251E-03 FS_EYE_B BL_EYE_B WL_EYE_B 2.3543E-01 -6.9136E-02 -1.9557E-03 SEPARATION BUBBLE GEOMETRY - WING/BODY/NACELLE/PYLON - FINE GRID FS_BUB BL_BUB WL_BUB 1.9812E-01 -9.4925E-02 1.0652E-02 FS_EYE_W BL_EYE_W WL_EYE_W 2.3734E-01 -7.7718E-02 -9.5079E-03 FS_EYE_B BL_EYE_B WL_EYE_B 2.4001E-01 -6.9765E-01 -9.6895E-05 CASE 2 DRAG POLAR - MEDIUM GRID (REQUIRED) --------------------------------- WING/BODY MACH ALPHA CL_TOT (min, max) CD_TOT (min, max) CD_PR CD_SF CD-CL2/PA CM_TOT (min, max) 0.75 -3.0 1.3989E-01 (steady) 1.8140E-02 (steady) 7.1621E-03 1.0978E-02 1.7480E-02 -1.5242E-01 (steady) 0.75 -2.0 2.5772E-01 (steady) 1.9698E-02 (steady) 8.7345E-03 1.0964E-02 1.7459E-02 -1.4831E-01 (steady) 0.75 -1.5 3.1638E-01 (steady) 2.0921E-02 (steady) 9.9716E-03 1.0949E-02 1.7547E-02 -1.4653E-01 (steady) 0.75 -1.0 3.7458E-01 (steady) 2.2406E-02 (steady) 1.1480E-02 1.0926E-02 1.7676E-02 -1.4424E-01 (steady) 0.75 0.0 4.9355E-01 (steady) 2.6232E-02 (steady) 1.5386E-02 1.0845E-02 1.8020E-02 -1.3948E-01 (steady) 0.75 1.0 6.1835E-01 (steady) 3.2345E-02 (steady) 2.1606E-02 1.0739E-02 1.9455E-02 -1.3310E-01 (steady) 0.75 1.5 6.7907E-01 (steady) 3.7001E-02 (steady) 2.6375E-02 1.0626E-02 2.1455E-02 -1.2963E-01 (steady) WING/BODY/NACELLE/PYLON MACH ALPHA CL_TOT (min, max) CD_TOT (min, max) CD_PR CD_SF CD-CL2/PA CM_TOT (min, max) 0.75 -3.0 9.9546E-02 (steady) 2.5656E-02 (steady) 1.2559E-02 1.3097E-02 2.5322E-02 -1.6855E-01 (steady) 0.75 -2.0 2.0386E-01 (steady) 2.4996E-02 (steady) 1.1907E-02 1.3089E-02 2.3595E-02 -1.6045E-01 (steady) 0.75 -1.5 2.5624E-01 (steady) 2.5157E-02 (steady) 1.2081E-02 1.3076E-02 2.2943E-02 -1.5626E-01 (steady) 0.75 -1.0 3.1083E-01 (steady) 2.5766E-02 (steady) 1.2705E-02 1.3061E-02 2.2508E-02 -1.5248E-01 (steady) 0.75 0.0 4.2931E-01 (steady) 2.8157E-02 (steady) 1.5140E-02 1.3017E-02 2.1942E-02 -1.4429E-01 (steady) 0.75 0.5 4.9393E-01 (steady) 3.0060E-02 (steady) 1.7081E-02 1.2978E-02 2.1834E-02 -1.3977E-01 (steady) 0.75 1.0 5.5630E-01 (steady) 3.2818E-02 (steady) 1.9899E-02 1.2919E-02 2.2383E-02 -1.3489E-01 (steady) 0.75 1.5 6.1860E-01 (steady) 3.6602E-02 (steady) 2.3778E-02 1.2824E-02 2.3699E-02 -1.2950E-01 (steady) UPPER SURFACE TRANSITION LOCATIONS (% CHORD) XROOT XKINK XE.844 XTIP ??. ??. ??. ??. LOWER SURFACE TRANSITION LOCATION (% CHORD) XLO ??.