#++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ # # DPW-VI FORCE & MOMENT DATA SUBMITTAL FORM (Version 4 - 22 April 2016) # # Due 14 MAY 2016 # # XXX: First-author participant's last name + specific identifier if submitting # multiple grid types, soln methods, turb models, etc. # EXAMPLES: JonesG-CommonMB-SST-1 # JonesG-CommonOverset-SA-1 # JonesG-CommonOverset-SA-2 # JonesG-CommonHex-kw-1 # JonesG-CommonHybrid-ke-1 # JonesG-CommonPrism-SST-1 # JonesG-Custom-SA-1 # etc. # # NOMENCLATURE: # GRID_LEVEL: Level of grid refinement (1-6) # GRID_SIZE: Number of grid nodes or cells # GRIDFAC: 1/GRID_SIZE**2/3 # ALPHA: Angle of Attack, deg # CL: Coefficient of Lift (total) (L/(0.5*rho_inf*U_inf^2*A) ) # CD: Coefficient of Drag (total) (D/(0.5*rho_inf*U_inf^2*A) ) # CM: Coefficient of Pitching Moment (total) (M/(0.5*rho_inf*U_inf^2*A*c)) (+ nose-up) # CD_PR: Surface-Pressure Integrated Drag Coefficient # CD_SF: Skin-Friction Integrated Drag Coefficient # CD-CL2/PA: CD_TOT - (CL_TOT*CL_TOT)/(PI*AR) # *_TOT: Total Configuration Force/Moment # *_WING: Wing Component Force/Moment # *_FUS: Fuselage Component Force/MomenT # MASSFLOW: Mass flow through nacelle - Integral RHO*U dA # Over an X=1150 (or any other cut-planeā€Ž of the inner flow path of the nacelle) - Units: Slugs/sec # # Here is a link to the tecplot add-on for designating the collection of nodes from a slice to use for the mass flow integration, # an example of it use is included in the zip file. Works only for newer Windows or Linux versions of Tecplot 360. # ftp://ftp.tecplot.com/outgoing/ExtractConnectedNodes.zip # # REFERENCE VALUES: # 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 = 468.75 inches # z moment center = 177.95 inches # Aspect Ratio, AR = 9.00 # # FLOW CONDITIONS: # Mach Number: 0.85 # Reynolds Number: 5.0 million (based on Cref=275.80) # Freestream Temp: 100 deg F # # 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" VARIABLES = "GRID_LEVEL" "GRID_SIZE" "GRIDFAC" "ALPHA" "CL_TOT" "CD_TOT" "CD_PR" "CD_SF" "CD-CL2/PA" "CM_TOT" "CL_WING" "CD_WING" "CM_WING" "CL_FUS" "CD_FUS" "CM_FUS" "MASSFLOW" #--------------------------------------------------- # PARTICIPANT, GRID, AND SOLVER INFORMATION #--------------------------------------------------- DATASETAUXDATA Name = "Name of Participant" DATASETAUXDATA SubmissionDate = "Date of Submission" DATASETAUXDATA SolverName = "?" DATASETAUXDATA BasicAlgorithm = "?" DATASETAUXDATA TurbulenceModel = "SA, SA-RC, SA-la, SST, SST-2003, Wilcox1998k-w, EARSMko2005, etc." DATASETAUXDATA Miscellaneous = "???" DATASETAUXDATA GridId = "CommonMB, CommonOverset, CommonHex, CommonHybrid, CommonPrism, Custom, etc." #------------------------------------------------------------------------------- #CASE 2: SINGLE-POINT GRID CONVERGENCE STUDY # REQUIRED: L2, L3, L4, L5 (COARSE, MEDIUM, FINE, EXTRAFINE) GRIDS # OPTIONAL: L1, L6 (TINY, SUPERFINE) GRIDS # OPTIONAL: INDIVIDUAL COMPONENT FORCES AND MOMENTS #------------------------------------------------------------------------------- +----------------------- OPTIONAL -------------------------+ ZONE T="XXX - Case2A: WING/BODY SINGLE-POINT GRID CONVERGENCE STUDY" AUXDATA CFDCASE = "CASE2A" AUXDATA ID = "id - to be specified by the committee upon receipt" AUXDATA Name = "Name of Participant" AUXDATA SolverName = "?" AUXDATA TurbulenceModel = "SA, SA-RC, SA-la, SST, SST-2003, Wilcox1998k-w, EARSMko2005, etc." AUXDATA GridId = "CommonMB, CommonOverset, CommonHex, CommonHybrid, CommonPrism, Custom, etc." 1 ????????? ?.???? ?.???? 0.50???? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 2 ????????? ?.???? ?.???? 0.50???? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 3 ????????? ?.???? ?.???? 0.50???? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 4 ????????? ?.???? ?.???? 0.50???? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 5 ????????? ?.???? ?.???? 0.50???? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 6 ????????? ?.???? ?.???? 0.50???? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 ZONE T="XXX - Case2B: WING/BODY/NACELLE/PYLON SINGLE-POINT GRID CONVERGENCE STUDY" AUXDATA CFDCASE = "CASE2B" AUXDATA ID = "id - to be specified by the committee upon receipt" AUXDATA Name = "Name of Participant" AUXDATA SolverName = "?" AUXDATA TurbulenceModel = "SA, SA-RC, SA-la, SST, SST-2003, Wilcox1998k-w, EARSMko2005, etc." AUXDATA GridId = "CommonMB, CommonOverset, CommonHex, CommonHybrid, CommonPrism, Custom, etc." 1 ????????? ?.???? ?.???? 0.50???? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.????? 2 ????????? ?.???? ?.???? 0.50???? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.????? 3 ????????? ?.???? ?.???? 0.50???? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.????? 4 ????????? ?.???? ?.???? 0.50???? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.????? 5 ????????? ?.???? ?.???? 0.50???? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.????? 6 ????????? ?.???? ?.???? 0.50???? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.????? #------------------------------------------------------------------------------- #CASE 3-6: WING-BODY BUFFET STUDY (L3, MEDIUM GRID) # REQUIRED: ALPHA = 2.50, 2.75, 3.00, 3.25, 3.50, 3.75, 4.00 # OPTIONAL: ADDITIONAL ANGLES # OPTIONAL: INDIVIDUAL COMPONENT FORCES AND MOMENTS #------------------------------------------------------------------------------- +----------------------- OPTIONAL -------------------------+ ZONE T="XXX - Case3: WING-BODY STATIC AEROELASTIC BUFFET STUDY" AUXDATA CFDCASE = "CASE3" AUXDATA ID = "id - to be specified by the committee upon receipt" AUXDATA Name = "Name of Participant" AUXDATA SolverName = "?" AUXDATA TurbulenceModel = "SA, SA-RC, SA-la, SST, SST-2003, Wilcox1998k-w, EARSMko2005, etc." AUXDATA GridId = "CommonMB, CommonOverset, CommonHex, CommonHybrid, CommonPrism, Custom, etc." 3 ????????? ?.???? 2.5000 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 3 ????????? ?.???? 2.7500 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 3 ????????? ?.???? 3.0000 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 3 ????????? ?.???? 3.2500 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 3 ????????? ?.???? 3.5000 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 3 ????????? ?.???? 3.7500 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 3 ????????? ?.???? 4.0000 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 ZONE T="XXX - Case4: WING-BODY GRID ADAPTION BUFFET STUDY" AUXDATA CFDCASE = "CASE4" AUXDATA ID = "id - to be specified by the committee upon receipt" AUXDATA Name = "Name of Participant" AUXDATA SolverName = "?" AUXDATA TurbulenceModel = "SA, SA-RC, SA-la, SST, SST-2003, Wilcox1998k-w, EARSMko2005, etc." AUXDATA GridId = "CommonMB, CommonOverset, CommonHex, CommonHybrid, CommonPrism, Custom, etc." 3 ????????? ?.???? 2.5000 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 3 ????????? ?.???? 2.7500 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 3 ????????? ?.???? 3.0000 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 3 ????????? ?.???? 3.2500 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 3 ????????? ?.???? 3.5000 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 3 ????????? ?.???? 3.7500 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 3 ????????? ?.???? 4.0000 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 ZONE T="XXX - Case5: WING-BODY COUPLED AEROELASTIC BUFFET STUDY" AUXDATA CFDCASE = "CASE5" AUXDATA ID = "id - to be specified by the committee upon receipt" AUXDATA Name = "Name of Participant" AUXDATA SolverName = "?" AUXDATA TurbulenceModel = "SA, SA-RC, SA-la, SST, SST-2003, Wilcox1998k-w, EARSMko2005, etc." AUXDATA GridId = "CommonMB, CommonOverset, CommonHex, CommonHybrid, CommonPrism, Custom, etc." 3 ????????? ?.???? 2.5000 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 3 ????????? ?.???? 2.7500 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 3 ????????? ?.???? 3.0000 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 3 ????????? ?.???? 3.2500 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 3 ????????? ?.???? 3.5000 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 3 ????????? ?.???? 3.7500 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 3 ????????? ?.???? 4.0000 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 ZONE T="XXX - Case6: WING-BODY PARTICIPANT GRID BUFFET STUDY" AUXDATA CFDCASE = "CASE6" AUXDATA ID = "id - to be specified by the committee upon receipt" AUXDATA Name = "Name of Participant" AUXDATA SolverName = "?" AUXDATA TurbulenceModel = "SA, SA-RC, SA-la, SST, SST-2003, Wilcox1998k-w, EARSMko2005, etc." AUXDATA GridId = "CommonMB, CommonOverset, CommonHex, CommonHybrid, CommonPrism, Custom, etc." 3 ????????? ?.???? 2.5000 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 3 ????????? ?.???? 2.7500 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 3 ????????? ?.???? 3.0000 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 3 ????????? ?.???? 3.2500 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 3 ????????? ?.???? 3.5000 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 3 ????????? ?.???? 3.7500 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999 3 ????????? ?.???? 4.0000 ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? ?.??????? ?.?????? ?.?????? -999