#+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ # # HLPW-4 Cp & Cf Grid Convergence DATA SUBMITTAL FORM Case 1b (Version 2), January 13, 2021 # # CASE 1b is a mesh convergence study for the HL-CRM nominal 40/37 configuration at alpha=7.05 deg. # For RANS, this case should be run FULLY TURBULENT (no forced transition) in FREE AIR (no tunnel walls). # # NOMENCLATURE: # N: Number of unknowns (grid points for node-centered code, grid cells for cell-centered code) # X, Y, Z: Coordinates of each computational point on the pressure cut in inches # CP: Coefficient of pressure - give mean if not converged to steady-state # CF: Skin-friction coefficient at wall = tau_w/(freestream dynamic pressure) # - give mean if not converged to steady-state # CFX, CFY, CFZ: Components of skin-friction coefficient at wall # - give mean if not converged to steady-state # # ALPHA: Angle of attack, deg. # MAC: Mean aerodynamic chord = 275.8 inches # FT: Fully Turbulent # # XXX: Participant ID (To be assigned by HLPW committee) # # slat-Z: Indicates the slat Z plane, where Z = A, B, C, ... , H # wing-Z: Indicates the wing Z plane, where Z = A, B, C, ... , H # flap-Z: Indicates the flap Z plane, where Z = A, B, C, ... , H # The spanwise cut locations for HL-CRM (all elements stowed) are: # (see website for details on how to extract appropriately for deployed config) # A: y= 174.5 inches (eta approx 0.15) # B: y= 277.5 inches (eta approx 0.24) # C: y= 380.5 inches (eta approx 0.33) # D: y= 483.5 inches (eta approx 0.42) # E: y= 638.0 inches (eta approx 0.55) # F: y= 792.5 inches (eta approx 0.69) # G: y= 947.0 inches (eta approx 0.82) # H: y=1050.0 inches (eta approx 0.91) # # FLOW CONDITIONS: # Angle of Attack: 7.05 deg # Mach Number: 0.2 # Reynolds Number: 5.49 million (based on MAC) # Freestream Temp: 521 R # Freestream Static Pressure: 24.67 psi # # NOTES: 1. All numerical data fields can be free-formatted # 2. Please use at least 5 decimal places in the numerical values for CL CD CM # 3. If data are NOT provided, please fill data fields with a numerical value of "-999" # 4. If not converged to steady-state (i.e., if run with a scale-resolving simulation # or run time-accurately), give mean values of everything # #+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ TITLE = "XXX" # <----- Optional -----> VARIABLES = "N" "X" "Y" "Z" "CP" "CF" "CFX" "CFY" "CFZ" # The following section is for grid A: ZONE T="XXX slat-A case1b A-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-A case1b A-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-A case1b A-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-B case1b A-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-B case1b A-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-B case1b A-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-C case1b A-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-C case1b A-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-D case1b A-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-D case1b A-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-D case1b A-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-E case1b A-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-E case1b A-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-E case1b A-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-F case1b A-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-F case1b A-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-F case1b A-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-G case1b A-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-G case1b A-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-H case1b A-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-H case1b A-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 # The following section is for grid B: ZONE T="XXX slat-A case1b B-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-A case1b B-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-A case1b B-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-B case1b B-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-B case1b B-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-B case1b B-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-C case1b B-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-C case1b B-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-D case1b B-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-D case1b B-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-D case1b B-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-E case1b B-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-E case1b B-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-E case1b B-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-F case1b B-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-F case1b B-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-F case1b B-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-G case1b B-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-G case1b B-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-H case1b B-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-H case1b B-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 # The following section is for grid C: ZONE T="XXX slat-A case1b C-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-A case1b C-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-A case1b C-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-B case1b C-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-B case1b C-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-B case1b C-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-C case1b C-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-C case1b C-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-D case1b C-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-D case1b C-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-D case1b C-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-E case1b C-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-E case1b C-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-E case1b C-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-F case1b C-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-F case1b C-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-F case1b C-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-G case1b C-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-G case1b C-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-H case1b C-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-H case1b C-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 # The following section is for grid D: ZONE T="XXX slat-A case1b D-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-A case1b D-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-A case1b D-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-B case1b D-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-B case1b D-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-B case1b D-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-C case1b D-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-C case1b D-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-D case1b D-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-D case1b D-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-D case1b D-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-E case1b D-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-E case1b D-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-E case1b D-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-F case1b D-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-F case1b D-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-F case1b D-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-G case1b D-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-G case1b D-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-H case1b D-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-H case1b D-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 # The following section is for grid E: ZONE T="XXX slat-A case1b E-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-A case1b E-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-A case1b E-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-B case1b E-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-B case1b E-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-B case1b E-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-C case1b E-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-C case1b E-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-D case1b E-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-D case1b E-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-D case1b E-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-E case1b E-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-E case1b E-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-E case1b E-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-F case1b E-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-F case1b E-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-F case1b E-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-G case1b E-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-G case1b E-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-H case1b E-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-H case1b E-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 # The following section is for grid F: ZONE T="XXX slat-A case1b F-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-A case1b F-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-A case1b F-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-B case1b F-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-B case1b F-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-B case1b F-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-C case1b F-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-C case1b F-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-D case1b F-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-D case1b F-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-D case1b F-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-E case1b F-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-E case1b F-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-E case1b F-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-F case1b F-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-F case1b F-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX flap-F case1b F-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-G case1b F-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-G case1b F-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX slat-H case1b F-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999 ZONE T="XXX wing-H case1b F-mesh a7.05 freeair FT" -999 -999 -999 -999 -999 -999 -999 -999 -999