#++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ # # HiLiftPW-2 Velocity DATA SUBMITTAL FORM Case 3a (Version 1), March 2013 # # CASE 3 is an optional Reynolds number study at 8 different angles-of-attack each. # Config 5 (including Slat Tracks and Flap Track Fairings and slat pressure tube bundles) should be used. # A comparable *Medium* mesh density from the Grid Convergence Study should be used. # The case can be run either fully turbulent or with transition specified/computed (please specify which!!!). # # This data file only asks for a subset of information to be reported: AoA=7, 18.5, and 21 only. # # NOMENCLATURE: # ALPHA: Angle of attack, deg. # FT: Fully Turbulent # TR: Transition specified or computed # 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 # # XXX: Participant ID (To be assigned by HiLiftPW-1 workshop committee) # # FLOW CONDITIONS CASE 3a: # Mach Number: 0.175 # Reynolds Number: 1.35 million (based on MAC) # Freestream Temp: 298.6 K (537.48 R) # Freestream Static Pressure: 100700 Pa (14.6053 psi) # # NOTES: 1. All numerical data fields can be free-formatted # 2. Please use at least 3 decimal places in the numerical values for velocity # 3. If optional data is NOT provided, please fill data fields with a numerical value of "-999" # 4. Results are requested for both medium and fine grids # #++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ TITLE = "XXX" VARIABLES = "X" "Y" "Z" "u/Uinf" "v/Uinf" "w/Uinf" #----------------------------------------------------------------------------------- # ALPHA 7: #----------------------------------------------------------------------------------- ZONE T="XXX case3a a7 medium, p1, wB, line1" # extract along Z at X=1162.58, Y=246.386, from wing upper surface to at least 59mm high above surface 1162.58 246.386 -999 -999 -999 -999 ZONE T="XXX case3a a7 medium, p1, wB, line2" # extract along Z at X=1181.87, Y=246.386, from wing upper surface to at least 59mm high above surface 1181.87 246.386 -999 -999 -999 -999 ZONE T="XXX case3a a7 medium, p1, wC, line1" # extract along Z at X=1296.28, Y=246.386, from wing upper surface to at least 59mm high above surface 1296.28 246.386 -999 -999 -999 -999 ZONE T="XXX case3a a7 medium, p1, wD, line1" # extract along Z at X=1461.48, Y=246.386, from wing upper surface to at least 59mm high above surface 1461.48 246.386 -999 -999 -999 -999 ZONE T="XXX case3a a7 medium, p2, wB, line1" # extract along Z at X=1635.09, Y=979.596, from wing upper surface to at least 59mm high above surface 1635.09 979.596 -999 -999 -999 -999 ZONE T="XXX case3a a7 medium, p2, wB, line2" # extract along Z at X=1648.20, Y=979.596, from wing upper surface to at least 59mm high above surface 1648.20 979.596 -999 -999 -999 -999 ZONE T="XXX case3a a7 medium, p2, wD, line1" # extract along Z at X=1749.74, Y=979.596, from wing upper surface to at least 59mm high above surface 1749.74 979.596 -999 -999 -999 -999 ZONE T="XXX case3a a7 medium, p2, wE, line1" # extract along Z at X=1821.37, Y=979.596, from flap upper surface to at least 59mm high above surface 1821.37 979.596 -999 -999 -999 -999 ZONE T="XXX case3a a7 medium, p2, wE, line2" # extract along Z at X=1846.71, Y=979.596, from flap upper surface to at least 59mm high above surface 1846.71 979.596 -999 -999 -999 -999 ZONE T="XXX case3a a7 medium, p3, wE, line1" # extract along Z at X=1921.73, Y=1223.999, from flap upper surface to at least 59mm high above surface 1921.73 1223.999 -999 -999 -999 -999 ZONE T="XXX case3a a7 medium, p3, wE, line2" # extract along Z at X=1944.93, Y=1223.999, from flap upper surface to at least 59mm high above surface 1944.93 1223.999 -999 -999 -999 -999 #----------------------------------------------------------------------------------- # ALPHA 18.5: #----------------------------------------------------------------------------------- ZONE T="XXX case3a a18.5 medium, p1, wB, line1" # extract along Z at X=1162.58, Y=246.386, from wing upper surface to at least 59mm high above surface 1162.58 246.386 -999 -999 -999 -999 ZONE T="XXX case3a a18.5 medium, p1, wB, line2" # extract along Z at X=1181.87, Y=246.386, from wing upper surface to at least 59mm high above surface 1181.87 246.386 -999 -999 -999 -999 ZONE T="XXX case3a a18.5 medium, p1, wC, line1" # extract along Z at X=1296.28, Y=246.386, from wing upper surface to at least 59mm high above surface 1296.28 246.386 -999 -999 -999 -999 ZONE T="XXX case3a a18.5 medium, p1, wD, line1" # extract along Z at X=1461.48, Y=246.386, from wing upper surface to at least 59mm high above surface 1461.48 246.386 -999 -999 -999 -999 ZONE T="XXX case3a a18.5 medium, p2, wB, line1" # extract along Z at X=1635.09, Y=979.596, from wing upper surface to at least 59mm high above surface 1635.09 979.596 -999 -999 -999 -999 ZONE T="XXX case3a a18.5 medium, p2, wB, line2" # extract along Z at X=1648.20, Y=979.596, from wing upper surface to at least 59mm high above surface 1648.20 979.596 -999 -999 -999 -999 ZONE T="XXX case3a a18.5 medium, p2, wD, line1" # extract along Z at X=1749.74, Y=979.596, from wing upper surface to at least 59mm high above surface 1749.74 979.596 -999 -999 -999 -999 ZONE T="XXX case3a a18.5 medium, p2, wE, line1" # extract along Z at X=1821.37, Y=979.596, from flap upper surface to at least 59mm high above surface 1821.37 979.596 -999 -999 -999 -999 ZONE T="XXX case3a a18.5 medium, p2, wE, line2" # extract along Z at X=1846.71, Y=979.596, from flap upper surface to at least 59mm high above surface 1846.71 979.596 -999 -999 -999 -999 ZONE T="XXX case3a a18.5 medium, p3, wE, line1" # extract along Z at X=1921.73, Y=1223.999, from flap upper surface to at least 59mm high above surface 1921.73 1223.999 -999 -999 -999 -999 ZONE T="XXX case3a a18.5 medium, p3, wE, line2" # extract along Z at X=1944.93, Y=1223.999, from flap upper surface to at least 59mm high above surface 1944.93 1223.999 -999 -999 -999 -999 #----------------------------------------------------------------------------------- # ALPHA 21: #----------------------------------------------------------------------------------- ZONE T="XXX case3a a21 medium, p1, wB, line1" # extract along Z at X=1162.58, Y=246.386, from wing upper surface to at least 59mm high above surface 1162.58 246.386 -999 -999 -999 -999 ZONE T="XXX case3a a21 medium, p1, wB, line2" # extract along Z at X=1181.87, Y=246.386, from wing upper surface to at least 59mm high above surface 1181.87 246.386 -999 -999 -999 -999 ZONE T="XXX case3a a21 medium, p1, wC, line1" # extract along Z at X=1296.28, Y=246.386, from wing upper surface to at least 59mm high above surface 1296.28 246.386 -999 -999 -999 -999 ZONE T="XXX case3a a21 medium, p1, wD, line1" # extract along Z at X=1461.48, Y=246.386, from wing upper surface to at least 59mm high above surface 1461.48 246.386 -999 -999 -999 -999 ZONE T="XXX case3a a21 medium, p2, wB, line1" # extract along Z at X=1635.09, Y=979.596, from wing upper surface to at least 59mm high above surface 1635.09 979.596 -999 -999 -999 -999 ZONE T="XXX case3a a21 medium, p2, wB, line2" # extract along Z at X=1648.20, Y=979.596, from wing upper surface to at least 59mm high above surface 1648.20 979.596 -999 -999 -999 -999 ZONE T="XXX case3a a21 medium, p2, wD, line1" # extract along Z at X=1749.74, Y=979.596, from wing upper surface to at least 59mm high above surface 1749.74 979.596 -999 -999 -999 -999 ZONE T="XXX case3a a21 medium, p2, wE, line1" # extract along Z at X=1821.37, Y=979.596, from flap upper surface to at least 59mm high above surface 1821.37 979.596 -999 -999 -999 -999 ZONE T="XXX case3a a21 medium, p2, wE, line2" # extract along Z at X=1846.71, Y=979.596, from flap upper surface to at least 59mm high above surface 1846.71 979.596 -999 -999 -999 -999 ZONE T="XXX case3a a21 medium, p3, wE, line1" # extract along Z at X=1921.73, Y=1223.999, from flap upper surface to at least 59mm high above surface 1921.73 1223.999 -999 -999 -999 -999 ZONE T="XXX case3a a21 medium, p3, wE, line2" # extract along Z at X=1944.93, Y=1223.999, from flap upper surface to at least 59mm high above surface 1944.93 1223.999 -999 -999 -999 -999