#++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ # # DPW-8/AePW-4 FORCE AND MOMENT SUBMITTAL FORM (Version 4 - September 19, 2024) # # Provide this file for steady-state or time-averaged force and moment coefficients # # # # Data Set Title XXX.YY: Replace "XXX.YY" in the zone titles with the following information # (Three-Digit Participant ID).(Two-Digit Submission ID) # XXX THREE-DIGIT PARTICIPANT ID: assigned by your working group leaders # YY TWO-DIGIT SUBMISSION ID: (self assigned) label a solver/grid/computational approach # EXAMPLE: 007.02 # # # NOMENCLATURE: # GRID_LEVEL: Level of grid refinement (1-6) # GRID_SIZE: Number of grid nodes or cells # GRIDFAC: 1/GRID_SIZE**2/3 # MACH: Freestream Mach Number # REY: Chord-Based Reynolds Number # ALPHA: Angle of Attack, deg # CL: Coefficient of Lift (total) (L/(0.5*rho_inf*U_inf^2*A) ) Provided to eight decimal points # CD: Coefficient of Drag (total) (D/(0.5*rho_inf*U_inf^2*A) ) Provided to nine decimal points # CM: Coefficient of Pitching Moment (total) (M/(0.5*rho_inf*U_inf^2*A*c)) (+ nose-up) Provided to eight decimal points # CD_PR: Surface-Pressure Integrated Drag Coefficient # CD_SF: Skin-Friction Integrated Drag Coefficient # *_TOT: Total Configuration Force/Moment # *_TAIL: Horizontal Tail Component Force/Moment # *_WING: Wing Component Force/Moment # *_FUS: Fuselage Component Force/Moment # *_NAC: Nacelle Component Force/Moment # *_PY: Pylon Component Force/Moment # CPU: CPU (or GPU) hours used # DT: Time Step Per Iteration # CTUSTART: Convective Time Unit at Which Averaging Began # CTUAVG: Number of Convective Time Units in Time-Averaging Phase # Q/E: Dynamic Pressure / Modulus of Elasticity # # DECIMAL POINTS: Please provide data in at least the number of decimal points listed below (?.???????? would have at least eight decimal points) # # OPTIONAL DATA: Enter -999 for any optional data you are not submitting # # REFERENCE VALUES: ONERA OAT15A (ONE CELL WIDE) # Planform ref area, A = Cref * span (span is grid dependent) # Mean aerodynamic chord, Cref = 230.00 mm # x moment center = 57.50 mm # y moment center = 0.00 mm # z moment center = 0.00 mm # # REFERENCE VALUES: Common Research Model # Planform ref area, A = 594720.00 inches^2 # Mean aerodynamic chord, Cref = 275.80 inches # Full-span length, B = 2313.50 inches # Semi-span length, BO2 = 1156.75 inches # x moment center = 1325.90 inches # y moment center = 0.00 inches # z moment center = 177.95 inches # Aspect Ratio, AR = 9.00 # # CONFIGURATION: ONERA OAT15A # CRMWB (Common Research Model Wing/Body) # CRMWBNP (Common Research Model Wing/Body/Nacelle/Pylon) # # NOTES: 1. All numerical data fields can be free-formatted. # 2. Please use at least 4 decimal places for coordinate values # 3. Please use at least 6 decimal places for coefficient values # 4. Only include one grid type, grid size, soln method, turb model, etc per form. # 5. Fill fields with value of -999 for data that are not available. # #++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ TITLE = "XXX.YY" # +----------------------------------------------------------------------- OPTIONAL ---------------------------------------------------------------------------------------------------------------------+ # Column 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 VARIABLES = "GRID_LEVEL" "GRID_SIZE" "GRID_FAC" "MACH" "REY" "ALPHA" "CL_TOT" "CD_TOT" "CM_TOT" "CL_WING" "CD_WING" "CM_WING" "CD_PR" "CD_SF" "CL_TAIL" "CD_TAIL" "CM_TAIL" "CL_FUS" "CD_FUS" "CM_FUS" "CL_NAC" "CD_NAC" "CM_NAC" "CL_PY" "CD_PY" "CM_PY" "CPU_Hours" "DELTAT" "CTUSTART" "CTUAVG" "Q/E" #--------------------------------------------------- # PARTICIPANT, GRID, AND SOLVER INFORMATION #--------------------------------------------------- DATASETAUXDATA ParticipantID = "Participant ID" DATASETAUXDATA SubmissionDate = "Date of Submission" DATASETAUXDATA Name = "Name of Participant" DATASETAUXDATA Email = "Email Address of Participant" DATASETAUXDATA Institution = "Name of your company/organization" DATASETAUXDATA SolverName = "Solver name used and version number" DATASETAUXDATA BasicAlgorithm = "RANS, URANS, DES, DDES, WMLES, etc." DATASETAUXDATA TurbulenceModel = "SA, SA-RC, SA-la, SST, SST-2003, Wilcox1998k-w, EARSMko2005, etc." DATASETAUXDATA GridId = "Multiblock, Overset, Hex, Hybrid, Prism, Custom, etc." DATASETAUXDATA Notes = "Any thing else you would like to add" #------------------------------------------------------------------------------- # REQUIRED: VEHICLE F&M # OPTIONAL: INDIVIDUAL COMPONENT FORCES AND MOMENTS #------------------------------------------------------------------------------- ZONE T="XXX.YY" AUXDATA Tstatic = "??" AUXDATA Deltat = "Time step for unstady schemes (optional)" AUXDATA GridFileName = "File name(s) of the grid(s) you used" AUXDATA Misc = "Any thing else you would like to add" ? ????????? ?.????? ?.???? ??.?? ?.????? ?.???????? ?.????????? ?.???????? ?.???????? ?.????????? ?.???????? ?.????????? ?.????????? ?.???????? ?.????????? ?.???????? ?.???????? ?.????????? ?.???????? ?.???????? ?.????????? ?.???????? ?.???????? ?.????????? ?.???????? ?????.? ?.????? ?.????? ?.????? ?.?????