DPW-III DPW-Wing Alone CASE-2 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 W1 W2 ---------------------------------------- Zones: Field Nodes: Field Cells: Boundary Nodes: Boundary Faces: BL 1st-Cell Size: BL Max-Growth Rate: BL Cells: Miscellaneous: CASE 2.A: SINGLE-POINT GRID CONVERGENCE STUDY - FINE GRID CP AND CF DISTRIBUTIONS ---------------------------------------------------------------------------------- DPW-W1 GRID_SIZE MACH ALPHA CL ????????. 0.76 0.5 ?.??? WING SECTION 1 Y/BO2 0.026 (Y = 20. mm) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 2 Y/BO2 0.157 (Y = 120. mm) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 3 Y/BO2 0.289 (Y = 220. mm) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 4 Y/BO2 0.420 (Y = 320. mm) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 5 Y/BO2 0.551 (Y = 420. mm) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 6 Y/BO2 0.682 (Y = 520. mm) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 7 Y/BO2 0.814 (Y = 620. mm) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 8 Y/BO2 0.945 (Y = 720. mm) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? DPW-W2 GRID_SIZE MACH ALPHA CL ????????. 0.76 0.5 ?.??? WING SECTION 1 Y/BO2 0.026 (Y = 20. mm) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 2 Y/BO2 0.157 (Y = 120. mm) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 3 Y/BO2 0.289 (Y = 220. mm) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 4 Y/BO2 0.420 (Y = 320. mm) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 5 Y/BO2 0.551 (Y = 420. mm) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 6 Y/BO2 0.682 (Y = 520. mm) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 7 Y/BO2 0.814 (Y = 620. mm) X/C CP CF CFX CFY CFZ ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? WING SECTION 8 Y/BO2 0.945 (Y = 720. mm) 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 (762.0 mm)