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# HiLiftPW-3 Grid Convergence 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:
# N: Total number of grid points (node-centered code) or grid cells (cell-centered code)
# CL: Coefficient of lift (total)
# CD: Coefficient of drag (total)
# CDp: Coefficient of drap (pressure component)
# CDv: Coefficient of drap (viscous component)
# minU_1.01: minimum U/Uref in the airfoil wake at x/c=1.01
# minU_1.80: minimum U/Uref in the airfoil wake at x/c=1.80
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# alpha: Angle of attack, deg.
# 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
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TITLE = "XXX"
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VARIABLES = "N","CL","CD","CDp","CDv","minU_1.01","minU_1.80"
ZONE T="XXX case 3, FT"
# L1 grid (finest)
-999 -999 -999 -999 -999 -999 -999
# L2 grid (2nd finest)
-999 -999 -999 -999 -999 -999 -999
# L3 grid (3rd finest)
-999 -999 -999 -999 -999 -999 -999
# L4 grid (4th finest)
-999 -999 -999 -999 -999 -999 -999