#+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
#
#   HLPW-4 DATA SUBMITTAL FORM (Version 2), January 13, 2021
#   Case 3 multielement CRM-HL airfoil VERIFICATION case - FORCES
#
#   Tecplot data file (if you do not have Tecplot, then provide column data following the format given here)
#
#       NOMENCLATURE:
#                  N:  Number of unknowns (total gridpoints for node-centered code or total cells for 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)
#
#                XXX:  participant ID (to be assigned by HLPW committee)
#
#    FLOW CONDITIONS:
#                 Mach Number: 0.2
#                       alpha: 16
#             Reynolds Number: 5.0 million (based on stowed airfoil chord)
#             Freestream Temp: 272.1 K
#             This case should be run FULLY TURBULENT (no forced transition).
#
#              NOTES: 1. All numerical data fields can be free-formatted
#                     2. Please use at least 5 decimal places for all numerical values
#                     3. One line for each grid level run (provide at least 4 grid levels)
#
#+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
TITLE = "turbulence model name inserted here"
VARIABLES = "N" "CL" "CD" "CDp" "CDv"
ZONE T="XXX"
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