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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
#
#              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