xref: /phasta/phSolver/Test_C/solver.inp (revision 595995161822a203c8467e0e4a253d7bd7d6df32)

# PHASTAC Version 1.0 Input File
#
#  Basic format is
#
#    Key Phrase  :  Acceptable Value (integer, double, logical, or phrase
#                                     list of integers, list of doubles )
#

# To find the Key Phrases, first look in input.config.  There you will
# find the default values for everything that is allowed to have a
# default. Some things are not allowed to default and must be entered
# in this file.  In most cases, the acceptable inputs also appear in
# the input.config file. To add acceptable inputs you should only have
# to modify:

#     input_fform.cpp :which matches the string and translates it to the
#                    parameter change. If it is a new parameter, you must
#                    modify:
#
#                      common.h (to carry new parameter through code)
#                      common_c.h (to carry the parameter from C to Fortran)
#
#
# In case it is not clear by now, # allows you to comment either from the
# beginning of the line or to the right as shown below.
#
#SOLUTION CONTROL
#{
     Equation of State :  Compressible
     Number of Timesteps:  10        #replaces nsteps(1) (ntseq wired =1)
     Time Step Size: 1.0               # Delt(1)
     Turbulence Model:  No-Model       #  No-Model iturb=0, RANS =-1  LES=1 #}

#MATERIAL PROPERTIES
#{
     Viscosity: 1.0e-2      # fills datmat (2 values REQUIRED if iLset=1)
#}

OUTPUT CONTROL
{
#     Number of Force Surfaces: 3
#     Surface ID's for Force Calculation: 1 2 3
     Number of Timesteps between Restarts: 10 #replaces nout/ntout
     Print Statistics: True          #False=> ioform=1, True=> ioform=2
#     Print Error Indicators: True       # F ierrcalc = 0, T ierrcalc = 1
}

#LINEAR SOLVER
#{
#     Solver Type: GMRES Matrix Free
#     Solver Type: GMRES EBE
     Number of Solves per Left-hand-side Formation: 2  #nupdat/LHSupd(1)
     ACUSIM Verbosity Level               : 0   #iverbose
     Tolerance on Momentum Equations: 1.0e-4                   # epstol(1)
     Tolerance on ACUSIM Pressure Projection: 1.0e-2           # prestol
#}

#DISCRETIZATION CONTROL
#{
#    Entropy Form of Pressure Constraint on Weight Space: 1  # 1 turns it on
     Basis Function Order: 1                 # ipord
     Time Integration Rule: Second Order    # Second Order sets rinf next
     Time Integration Rho Infinity: -1     # rinf(1) Only used for 2nd order
     Include Viscous Correction in Stabilization: False    # if p=1 idiff=1
                                                           # if p=2 idiff=2
     Quadrature Rule on Interior: 2           #int(1)
     Quadrature Rule on Boundary: 2           #intb(1)
     Lumped Mass Fraction on Left-hand-side: 1.0           # flmpl
     Lumped Mass Fraction on Right-hand-side: 1.0          # flmpr
#     Tau Matrix: Matrix-Mallet               #itau=1
#     Discontinuity Capturing:  DC-mallet      #Sets IDC to 1
     Tau Time Constant: 2.                      #dtsfct
     Tau C Scale Factor: 1                    # taucfct  best value depends  #}

TURBULENCE MODELING PARAMETERS
{
#	Dynamic Model Type : Standard   # adds zero to iturb       LES
#        Filter Integration Rule: 1  #ifrule adds ifrule-1 to iturb LES
#	Turbulence Wall Model Type: Effective Viscosity  #itwmod=2 RANSorLES
3	Velocity Averaging Steps : 500. # wtavei= 1/this           RANSorLES
3	Dynamic Model Averaging Steps : 500. # dtavei= 1/this      LES
3	Filter Width Ratio        : 6.  # fwr1                     LES
 	}
#
#STEP SEQUENCE
#{
      Step Construction  : 0 1    # this is the standard two iteration
#}