#++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
#
#   HiLiftPW-3 Cp & Cf DATA SUBMITTAL FORM Case 1d (Version 1), March 2017
#
#   CASE 1d is an optional case for the HL-CRM configuration - partially-sealed chord flap gap, using grid adaptation
#   The finest (adapted) result should be reported
#   Two ALPHAs (8 and 16 deg) are required.
#   This case should be run FULLY TURBULENT (no forced transition).
#
#       NOMENCLATURE:
#            X, Y, Z:   Coordinates of each computational point on the pressure cut in inches
#                 CP:   Coefficient of pressure
#                 CF:   Skin-friction coefficient at wall = tau_w/(freestream dynamic pressure) 
#      CFX, CFY, CFZ:   Components of skin-friction coefficient at wall 
#
#              ALPHA:   Angle of attack, deg.
#                MAC:   Mean aerodynamic chord = 275.8 inches
#                 FT:   Fully Turbulent
#
#                XXX:   Participant ID (To be assigned by HiLiftPW workshop committee)
#
#            wingXXX:   Indicates the XXX plane that cuts through ALL wing elements at that station, 
#                       where 0.XXX denotes an APPROXIMATE percent of span
#                       (the various elements - slat, main, flap - are not differentiated here)
#            The y=const cut locations for HL-CRM are:
#                       y=174.5 inches (eta=0.151)
#                       y=277.5 inches (eta=0.240)
#                       y=380.5 inches (eta=0.329)
#                       y=483.5 inches (eta=0.418)
#                       y=638.0 inches (eta=0.552)
#                       y=792.5 inches (eta=0.685)
#                       y=947.0 inches (eta=0.819)
#                       y=1050.0 inches (eta=0.908)
#
#    FLOW CONDITIONS:
#                 Mach Number: 0.2
#             Reynolds Number: 3.26 million (based on MAC)
#             Freestream Temp: 518.67 R (= 15.0 C = 59.0 F)
#  Freestream Static Pressure: 760.21 mmHg (= 14.70 psi)
#
#              NOTES: 1. All numerical data fields can be free-formatted
#                     2. Please use at least 5 decimal places for all numerical values
#                     3. If optional data is NOT provided, please fill data fields with a numerical value of "-999" 
#                     4. For the HL-CRM, all CP cuts are at constant y (on all elements)
#
#++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++

TITLE = "XXX"

#                            <----- Optional ----->
VARIABLES = "X" "Y" "Z" "CP" "CF" "CFX" "CFY" "CFZ"

# The following section is for ALPHA=8, adapted grid:
ZONE T="XXX wing151 a8 case1d adapted FT partialgap"
 -999 -999 -999   -999   -999 -999 -999 -999

ZONE T="XXX wing240 a8 case1d adapted FT partialgap"
 -999 -999 -999   -999   -999 -999 -999 -999

ZONE T="XXX wing329 a8 case1d adapted FT partialgap"
 -999 -999 -999   -999   -999 -999 -999 -999

ZONE T="XXX wing418 a8 case1d adapted FT partialgap"
 -999 -999 -999   -999   -999 -999 -999 -999

ZONE T="XXX wing552 a8 case1d adapted FT partialgap"
 -999 -999 -999   -999   -999 -999 -999 -999

ZONE T="XXX wing685 a8 case1d adapted FT partialgap"
 -999 -999 -999   -999   -999 -999 -999 -999

ZONE T="XXX wing819 a8 case1d adapted FT partialgap"
 -999 -999 -999   -999   -999 -999 -999 -999
 
ZONE T="XXX wing908 a8 case1d adapted FT partialgap"
 -999 -999 -999   -999   -999 -999 -999 -999

# The following section is for ALPHA=16, adapted grid:
ZONE T="XXX wing151 a16 case1d adapted FT partialgap"
 -999 -999 -999   -999   -999 -999 -999 -999

ZONE T="XXX wing240 a16 case1d adapted FT partialgap"
 -999 -999 -999   -999   -999 -999 -999 -999

ZONE T="XXX wing329 a16 case1d adapted FT partialgap"
 -999 -999 -999   -999   -999 -999 -999 -999

ZONE T="XXX wing418 a16 case1d adapted FT partialgap"
 -999 -999 -999   -999   -999 -999 -999 -999

ZONE T="XXX wing552 a16 case1d adapted FT partialgap"
 -999 -999 -999   -999   -999 -999 -999 -999

ZONE T="XXX wing685 a16 case1d adapted FT partialgap"
 -999 -999 -999   -999   -999 -999 -999 -999

ZONE T="XXX wing819 a16 case1d adapted FT partialgap"
 -999 -999 -999   -999   -999 -999 -999 -999
 
ZONE T="XXX wing908 a16 case1d adapted FT partialgap"
 -999 -999 -999   -999   -999 -999 -999 -999