#+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ # # HLPW-4 DATA SUBMITTAL FORM (Version 2), January 13, 2021 # Case 3 multielement CRM-HL airfoil VERIFICATION case - CP and CF_X # # Tecplot data file (if you do not have Tecplot, then provide column data following the format given here) # # NOMENCLATURE: # x/c: x/c location on body # z/c: z/c location on body # cp: surface pressure coefficient # cf_x: x-component of surface skin friction coefficient # c: stowed chordlength (=1 in reference geometry provided) # # XXX: participant ID (to be assigned by HLPW committee) # # FLOW CONDITIONS: # Mach Number: 0.2 # alpha: 16 # Reynolds Number: 5.0 million (based on stowed airfoil chord) # Freestream Temp: 272.1 K # This case should be run FULLY TURBULENT (no forced transition). # # NOTES: 1. All numerical data fields can be free-formatted # 2. Please use at least 5 decimal places for all numerical values # 3. Provide a separate zone for each element (slat, main, and flap) # 4. Also provide results from your finest 3 grids run: # 7 = finest grid # 6 = second-finest grid # 5 = third-finest grid # #+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ TITLE = "turbulence model name inserted here" VARIABLES = "x/c" "z/c" "cp" "cf_x" ZONE T="XXX, slat, grid 7" x.xxxxxxxx x.xxxxxxxx x.xxxxxxxx x.xxxxxxxx ZONE T="XXX, main, grid 7" x.xxxxxxxx x.xxxxxxxx x.xxxxxxxx x.xxxxxxxx ZONE T="XXX, flap, grid 7" x.xxxxxxxx x.xxxxxxxx x.xxxxxxxx x.xxxxxxxx ZONE T="XXX, slat, grid 6" x.xxxxxxxx x.xxxxxxxx x.xxxxxxxx x.xxxxxxxx ZONE T="XXX, main, grid 6" x.xxxxxxxx x.xxxxxxxx x.xxxxxxxx x.xxxxxxxx ZONE T="XXX, flap, grid 6" x.xxxxxxxx x.xxxxxxxx x.xxxxxxxx x.xxxxxxxx ZONE T="XXX, slat, grid 5" x.xxxxxxxx x.xxxxxxxx x.xxxxxxxx x.xxxxxxxx ZONE T="XXX, main, grid 5" x.xxxxxxxx x.xxxxxxxx x.xxxxxxxx x.xxxxxxxx ZONE T="XXX, flap, grid 5" x.xxxxxxxx x.xxxxxxxx x.xxxxxxxx x.xxxxxxxx