#++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
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#   HiLiftPW-3 Velocity and turb shear stress DATA SUBMITTAL FORM Case 3 (Version 1), March 2017
#
#   CASE 3 is a requested turbulence model verification study for a 2-D DSMA661 (Model A) airfoil wake
#   This case should be run FULLY TURBULENT (no forced transition).
#
#       NOMENCLATURE:
#                x/c:   Coordinates of extracted results in the wake
#                y/c:   Coordinates on extracted results in the wake
#             u/Uref:   u-velocity nondimensionalized by freestream
#          uv/Uref^2:   u'v' (turbulent shear stress) nondimensionalized by freestream velocity squared
#
#              alpha:   Angle of attack, deg.
#                  c:   Airfoil chord
#               Uref:   freestream reference velocity
#                 FT:   Fully Turbulent
#
#                XXX:   Participant ID (To be assigned by HiLiftPW workshop committee)
#
#    FLOW CONDITIONS:
#                 Mach Number: 0.088
#                       alpha: 0
#             Reynolds Number: 1.2 million (based on airfoil chord)
#             Freestream Temp: 540 R
#
#              NOTES: 1. All numerical data fields can be free-formatted
#                     2. Please use at least 5 decimal places for all numerical values
#                     3. Results on finest grid should be reported
#
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TITLE = "XXX"
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VARIABLES = "x/c","y/c","u/Uref","uv/Uref^2"
ZONE T="XXX case 3, FT, finest grid, x/c=1.01"
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ZONE T="XXX case 3, FT, finest grid, x/c=1.05"
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ZONE T="XXX case 3, FT, finest grid, x/c=1.20"
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ZONE T="XXX case 3, FT, finest grid, x/c=1.40"
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ZONE T="XXX case 3, FT, finest grid, x/c=1.80"
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ZONE T="XXX case 3, FT, finest grid, x/c=2.19"
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ZONE T="XXX case 3, FT, finest grid, x/c=3.00"
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