#++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ # # HiLiftPW-3 Velocity DATA SUBMITTAL FORM Case 2b (Version 1), March 2017 # # CASE 2b is an optional nacelle-OFF run of the JSM configuration, using grid adaptation # The finest (adapted) result should be reported # Six ALPHAs are required: 4.36, 10.47, 14.54, 18.58, 20.59, and 21.57. # This case can be run fully turbulent or with forced transition or with a transition prediction method. # # NOMENCLATURE: # X,Y,Z: Cartesian coordinates, in mm # u/Uinf: Velocity component in X-direction relative to freestream # v/Uinf: Velocity component in Y-direction relative to freestream # w/Uinf: Velocity component in Z-direction relative to freestream # # ALPHA: Angle of attack, deg. # MAC: Mean aerodynamic chord = 529.2 mm # # XXX: Participant ID (To be assigned by HiLiftPW workshop committee) # # FLOW CONDITIONS: # Mach Number: 0.172 # Reynolds Number: 1.93 million (based on MAC) # Freestream Temp: 551.79 R (=33.40 C = 92.12 F) # Freestream Static Pressure: 747.70 mmHg (= 14.458 psi) # # NOTES: 1. All numerical data fields can be free-formatted # 2. Please use at least 5 decimal places for all numerical values # 3. If optional data is NOT provided, please fill data fields with a numerical value of "-999" # 4. For the JSM, the CP cuts are NOT at constant y (see website for details on how to extract appropriately) # 5. This assumes that your half-plane geometry lies in the -Y sector; # adjust accordingly if your geometry is in the +Y sector # #++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ TITLE = "XXX" VARIABLES = "X" "Y" "Z" "u/Uinf" "v/Uinf" "w/Uinf" #----------------------------------------------------------------------------------- # ALPHA 4.36: #----------------------------------------------------------------------------------- ZONE T="XXX case2b a4.36 adapted, x=2707.51, y=-565.81, no nacelle" # extract along Z, from wing upper surface to at least above all wakes 2707.51 -565.81 -999 -999 -999 -999 ZONE T="XXX case2b a4.36 adapted, x=2906.34, y=-1295.41, no nacelle" # extract along Z, from wing upper surface to at least above all wakes 2906.34 -1295.41 -999 -999 -999 -999 #----------------------------------------------------------------------------------- # ALPHA 10.47: #----------------------------------------------------------------------------------- ZONE T="XXX case2b a10.47 adapted, x=2707.51, y=-565.81, no nacelle" # extract along Z, from wing upper surface to at least above all wakes 2707.51 -565.81 -999 -999 -999 -999 ZONE T="XXX case2b a10.47 adapted, x=2906.34, y=-1295.41, no nacelle" # extract along Z, from wing upper surface to at least above all wakes 2906.34 -1295.41 -999 -999 -999 -999 #----------------------------------------------------------------------------------- # ALPHA 14.54: #----------------------------------------------------------------------------------- ZONE T="XXX case2b a14.54 adapted, x=2707.51, y=-565.81, no nacelle" # extract along Z, from wing upper surface to at least above all wakes 2707.51 -565.81 -999 -999 -999 -999 ZONE T="XXX case2b a14.54 adapted, x=2906.34, y=-1295.41, no nacelle" # extract along Z, from wing upper surface to at least above all wakes 2906.34 -1295.41 -999 -999 -999 -999 #----------------------------------------------------------------------------------- # ALPHA 18.58: #----------------------------------------------------------------------------------- ZONE T="XXX case2b a18.58 adapted, x=2707.51, y=-565.81, no nacelle" # extract along Z, from wing upper surface to at least above all wakes 2707.51 -565.81 -999 -999 -999 -999 ZONE T="XXX case2b a18.58 adapted, x=2906.34, y=-1295.41, no nacelle" # extract along Z, from wing upper surface to at least above all wakes 2906.34 -1295.41 -999 -999 -999 -999 #----------------------------------------------------------------------------------- # ALPHA 20.59: #----------------------------------------------------------------------------------- ZONE T="XXX case2b a20.59 adapted, x=2707.51, y=-565.81, no nacelle" # extract along Z, from wing upper surface to at least above all wakes 2707.51 -565.81 -999 -999 -999 -999 ZONE T="XXX case2b a20.59 adapted, x=2906.34, y=-1295.41, no nacelle" # extract along Z, from wing upper surface to at least above all wakes 2906.34 -1295.41 -999 -999 -999 -999 #----------------------------------------------------------------------------------- # ALPHA 21.57: #----------------------------------------------------------------------------------- ZONE T="XXX case2b a21.57 adapted, x=2707.51, y=-565.81, no nacelle" # extract along Z, from wing upper surface to at least above all wakes 2707.51 -565.81 -999 -999 -999 -999 ZONE T="XXX case2b a21.57 adapted, x=2906.34, y=-1295.41, no nacelle" # extract along Z, from wing upper surface to at least above all wakes 2906.34 -1295.41 -999 -999 -999 -999