#+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
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#   HLPW-4 Iterative Convergence for Flap Deflection Effect DATA SUBMITTAL FORM Case 1a (Version 2), January 13, 2021
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#   CASE 1a is a study of flap effect for the HL-CRM configuration at 7.05 deg; 3 geometries should be run:
#       40/37 inboard/outboard flap (nominal)
#       37/34 inboard/outboard
#       43/40 inboard/outboard
#   REQUIRED: Please report results on your best (finest) mesh; the same mesh "level" should be used for all cases.
#   OPTIONAL: Include results on other mesh levels if you have them.
#   For RANS, this case should be run FULLY TURBULENT (no forced transition) in FREE AIR (no tunnel walls).
#
#       NOMENCLATURE:
#                  N:   Number of unknowns (grid points for node-centered code, grid cells for cell-centered code)
#               ITER:   Iteration or time step number (ITER1=first recorded time step, ITERn=last time step).
#                       ITERn-ITER1 should be long enough to show any range in variation of final forces and moments. 
#                       If no variation exists (i.e., steady-state reached), provide at least the final 25% of the 
#                       range of iterations used.
#               TIME:   if run time-accurately, this is the corresponding nondimensional time since you started
#                       the computation (t*U_freestream/MAC)
#                 CL:	Coefficient of lift (total)
#                 CD:	Coefficient of drag (total)
#                 CM:	Coefficient of pitching moment (CMy) about moment reference center (MRC) (total) 
#           RESIDM-n:   (Optional) Residual of selected mean-flow equation (n=equation number)
#           RESIDT-n:   (Optional) Residual of selected turbulence equation (n=equation number)
#
#                MAC:   Mean aerodynamic chord = 275.8 inches
#                 FT:   Fully Turbulent
#
#                XXX:	Participant ID (To be assigned by HLPW committee)
#
#    FLOW CONDITIONS:
#             Angle of Attack: 7.05 deg
#                 Mach Number: 0.2
#             Reynolds Number: 5.49 million (based on MAC)
#             Freestream Temp: 521 R
#  Freestream Static Pressure: 24.67 psi
#
#              NOTES: 1. All numerical data fields can be free-formatted
#                     2. Please use at least 5 decimal places in the numerical values for CL CD CM
#                     3. Please use scientific notation (e.g. 2.51e-6) in the numerical values for RESIDM-n and RESIDT-n
#                     4. Residuals are optional; as many residuals can be provided as desired (up to 5 for mean flow, 
#                        up to 7 for turbulence)
#                     5. If data are NOT provided, please fill data fields with a numerical value of "-999" 
#                     6. Indicate (using each DATASETAUXDATA) whether local-time-stepping or time-accurate method was used
#
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TITLE = "XXX"

#                                            <------------------------------------------------------------ OPTIONAL ----------------------------------------------------------->
VARIABLES = "N" "ITER" "TIME" "CL" "CD" "CM" "RESIDM-1" "RESIDM-2" "RESIDM-3" "RESIDM-4" "RESIDM-5" "RESIDT-1" "RESIDT-2" "RESIDT-3" "RESIDT-4" "RESIDT-5" "RESIDT-6" "RESIDT-7"

DATASETAUXDATA TIMESTEPPING_METHOD_40_37  = "local-time-stepping -or- time-accurate"
ZONE T="XXX case1a flap:40/37 ALPHA=7.05 freeair FT"
 -999 -999 -999   -999 -999 -999   -999 -999 -999 -999 -999 -999 -999 -999 -999 -999 -999 -999
 -999 -999 -999   -999 -999 -999   -999 -999 -999 -999 -999 -999 -999 -999 -999 -999 -999 -999
 -999 -999 -999   -999 -999 -999   -999 -999 -999 -999 -999 -999 -999 -999 -999 -999 -999 -999
# etc...

DATASETAUXDATA TIMESTEPPING_METHOD_37_34  = "local-time-stepping -or- time-accurate"
ZONE T="XXX case1a flap:37/34 ALPHA=7.05 freeair FT"
 -999 -999 -999   -999 -999 -999   -999 -999 -999 -999 -999 -999 -999 -999 -999 -999 -999 -999
 -999 -999 -999   -999 -999 -999   -999 -999 -999 -999 -999 -999 -999 -999 -999 -999 -999 -999
 -999 -999 -999   -999 -999 -999   -999 -999 -999 -999 -999 -999 -999 -999 -999 -999 -999 -999
# etc...

DATASETAUXDATA TIMESTEPPING_METHOD_43_40  = "local-time-stepping -or- time-accurate"
ZONE T="XXX case1a flap:43/40 ALPHA=7.05 freeair FT"
 -999 -999 -999   -999 -999 -999   -999 -999 -999 -999 -999 -999 -999 -999 -999 -999 -999 -999
 -999 -999 -999   -999 -999 -999   -999 -999 -999 -999 -999 -999 -999 -999 -999 -999 -999 -999
 -999 -999 -999   -999 -999 -999   -999 -999 -999 -999 -999 -999 -999 -999 -999 -999 -999 -999
# etc...

# Include other ZONES (with titles modified to reflect the content) if you are including results for additional mesh levels