#++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
#
#   Pressure TRAP WING SPECIAL SESSION DATA SUBMITTAL FORM Version 2, February 2012
#
#       NOMENCLATURE:
#            X, Y, Z:	Coordinates of each computational point on the pressure cut in full scales inches 
#                       (deployed high-lift elements)
#                 CP:	Coefficient of pressure (  (p-p_inf)/(0.5*rho_inf*U_inf^2)  )
#             slatXX:   Indicates the slatXX plane, where XX denotes an APPROXIMATE percent of span in the stowed 
#                       position, which does not account for a 0.95 inch shift in y to align the base of the metric 
#                       standoff to the computational symmetry plane used for CFD (see file 
#                       extraction.planes.deployed-config1.txt for locations of extraction planes in terms of the 
#                       given deployed geometry; Tecplot macro files are also available to help you extract
#                       results appropriately for this configuration)
#             mainXX:   Indicates the main-wing mainXX plane (see extraction.planes.deployed-config1.txt or
#                       Tecplot macro files)
#             flapXX:   Indicates the flapXX plane (see extraction.planes.deployed-config1.txt or
#                       Tecplot macro files)
#        flapfwdspan:   Indicates forward row running out the span on the upper flap surface (see 
#                       extraction.planes.deployed-config1.txt or Tecplot macro files)
#             AoA-BB:   Indicates the angle of attack (e.g., AoA-13 = alpha 13 deg)
#
#                XXX:   First-author participant's last name + specific identifier if submitting
#                       multiple grid sizes, soln methods, turb models, etc.
#                       EXAMPLES:  JonesG-fine-SA
#                                  JonesG-med-SA
#                                  JonesG-med-SST
#                                  JonesG-nobrackets
#                                  JonesG-brackets
#
#    FLOW CONDITIONS:
#                 Mach Number: 0.2
#             Reynolds Number: 4.3 million (based on MAC)
#             Freestream Temp: 520 deg R
# Freestream Dynamic Pressure: 58 psf
#
#              NOTES: 1. Particularly of interest are CP data along 50% span, 85% span, and flapfwdspan at 
#                        AoA=13 and 28 deg. However, feel free to provide other CP data if desired (see 
#                        separate HiLiftPW-1 information for locations).
#                     2. All numerical data fields can be free-formatted.
#                     3. Please use at least 4 decimal places in all numerical values.
#                     4. Only include one grid-size, soln method, turb model, etc per form.
#                     5. Fill fields with value of -999 for data that are not available.
#
#++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++

TITLE = "XXX"
#
#   PARTICIPANT INFO:
#--------------------
#              Email:  
#              Phone:  
#            Address:  
#            Address:  
#            Address:  
#            Address:  
#            Address:  
#            Address:  
#
#  SOLVER INFORMATION (submit 1 form per method used)
#----------------------------------------------------
#        Solver Name:
#        Solver Vers:
#        Method Name:  
#    Basic Algorithm:  
#   Turbulence Model:  
#      Miscellaneous:  
#
#    GRID INFORMATION
#--------------------
#Grid-Generator Name:  
#Grid-Generator Vers:  
#          Grid Type:  
#
# GRID SIZE USED (submit 1 form per gridsize used)
#-------------------------------------------------
#              Zones:  
#        Field Nodes:  
#        Field Cells:  
#     Boundary Nodes:  
#     Boundary Faces:  
#   BL 1st-Cell Size:  
# BL Max-Growth Rate:  
#           BL Cells:  
#      Miscellaneous:  
#
# OTHER SPECIFICS (submit 1 form per methodology used)
#-----------------------------------------------------
# Are brackets included?
# Is transition modeled? How?
# Are walls included?
# Other:
#
# SOLUTION INFORMATION
#---------------------
#  Computer Platform:  
#       # Processors:  
#   Operating System:  
#           Compiler:  
#Typical RunTime CPU:  
#Run Time Wall-Clock:  
#Memory Requirements:  
#      Miscellaneous:  

VARIABLES = "X" "Y" "Z" "CP"

ZONE T="XXX slat50 AoA-13"
-999 -999 -999 -999

ZONE T="XXX main50 AoA-13"
-999 -999 -999 -999

ZONE T="XXX flap50 AoA-13"
-999 -999 -999 -999

ZONE T="XXX slat85 AoA-13"
-999 -999 -999 -999

ZONE T="XXX main85 AoA-13"
-999 -999 -999 -999

ZONE T="XXX flap85 AoA-13"
-999 -999 -999 -999

ZONE T="XXX flapfwdspan AoA-13"
-999 -999 -999 -999

ZONE T="XXX slat50 AoA-28"
-999 -999 -999 -999

ZONE T="XXX main50 AoA-28"
-999 -999 -999 -999

ZONE T="XXX flap50 AoA-28"
-999 -999 -999 -999

ZONE T="XXX slat85 AoA-28"
-999 -999 -999 -999

ZONE T="XXX main85 AoA-28"
-999 -999 -999 -999

ZONE T="XXX flap85 AoA-28"
-999 -999 -999 -999

ZONE T="XXX flapfwdspan AoA-28"
-999 -999 -999 -999
etc...

more ZONES if desired (label appropriately)...