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# HiLiftPW-3 Velocity and turb shear stress DATA SUBMITTAL FORM Case 3 (Version 1), March 2017
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# 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).
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# 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
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# alpha: Angle of attack, deg.
# c: Airfoil chord
# Uref: freestream reference velocity
# FT: Fully Turbulent
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# XXX: Participant ID (To be assigned by HiLiftPW workshop committee)
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# FLOW CONDITIONS:
# Mach Number: 0.088
# alpha: 0
# Reynolds Number: 1.2 million (based on airfoil chord)
# Freestream Temp: 540 R
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# 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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