DPW-III DLR-F6 CASE-1 CP Data Form ---------------------------------- Date: [Due 28 APR 2006] PARTICIPANT INFORMATION ----------------------- Name: Email: Phone: Address: Address: Address: Address: Address: Address: SOLVER INFORMATION -------------------- Method Name: Basic Algorithm: Turbulence Model: Miscellaneous: GRID INFORMATION -------------------- Grid-Generator Name: Grid Type: FINE GRID SIZE WB WBF ---------------------------------------- Zones: Field Nodes: Field Cells: Boundary Nodes: Boundary Faces: BL 1st-Cell Size: BL Max-Growth Rate: BL Cells: Miscellaneous: CASE 1.A: SINGLE-POINT GRID CONVERGENCE STUDY - FINE GRID CP AND CF DISTRIBUTIONS ---------------------------------------------------------------------------------- WING/BODY GRID_SIZE MACH ALPHA ????????. 0.75 ?.??? WING SECTION 1 Y/BO2 0.15 (Y = 0.08785 m) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 2 Y/BO2 0.239 (Y = 0.13987 m) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 3 Y/BO2 0.331 (Y = 0.19453 m) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 4 Y/BO2 0.377 (Y = 0.22156 m) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 5 Y/BO2 0.411 (Y = 0.24037 m) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 6 Y/BO2 0.514 (Y = 0.30090 m) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 7 Y/BO2 0.638 (Y = 0.37319 m) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 8 Y/BO2 0.847 (Y = 0.49602 m) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING/BODY/FX2B-FAIRING GRID_SIZE MACH ALPHA ????????. 0.75 ?.??? WING SECTION 1 Y/BO2 0.15 (Y = 0.08785 m) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 2 Y/BO2 0.239 (Y = 0.13987 m) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 3 Y/BO2 0.331 (Y = 0.19453 m) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 4 Y/BO2 0.377 (Y = 0.22156 m) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 5 Y/BO2 0.411 (Y = 0.24037 m) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 6 Y/BO2 0.514 (Y = 0.30090 m) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 7 Y/BO2 0.638 (Y = 0.37319 m) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 8 Y/BO2 0.847 (Y = 0.49602 m) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 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. * GRID_SIZE (F10.0) Number of grid nodes or cells Include as many X/C, CP pairs as necessary for each location * X/C (F12.4) X location on wing non-dimensionalized by local chord * CP (F12.4) Coefficient of pressure * CF (F12.6) Skin-friction Coefficient at wall = tauw/(freestream dynamic pressure) * CFX, CFY, CFZ (F12.6) Components of skin-friction Coefficient at wall * BO2 Semispan (585.647 mm)