POSSIBLE VALUES= 2 --> 2D problem
3 --> 3D problem
POSSIBLE VALUES= 0 --> disabled statistics collection
1 --> enabled statistics collection (expensive)
POSSIBLE VALUES= 0 --> default values
1 --> jacobi for DDES
11 --> matrix free lu-sgs for DDES
9 --> jacobi for RANS
91 --> matrix free lu-sgs for RANS
POSSIBLE VALUES= 1 --> Navier-Stokes
2 --> Euler
3 --> Linear Advection equation
4 --> Gradient approximation sample equation
-1 --> Multicomponent Euler equations
POSSIBLE VALUES= 0 --> Deactivated
1 --> Active
POSSIBLE VALUES= 0 --> DECOUPLED (DEFAULT)
1 --> COUPLED
POSSIBLE VALUES= 0 --> DEACTIVATED
1,2,3,..,N --> As many required, but only the first one is written in output file
POSSIBLE VALUES= --> Any positive value
POSSIBLE VALUES= --> Any value
POSSIBLE VALUES= --> Any value
POSSIBLE VALUES= --> Any value
POSSIBLE VALUES= --> Any positive value
-1 --> It will set pressure at P=RRES/GAMMA,
resulting in SPEED OF SOUND=1, AND Ufreestream=Mach number
POSSIBLE VALUES= --> ANY VALUE
SELECT WITH RESPECT TO WHICH AXIS THE ANGLE OF ATTACK IS DEFINED (XY,XZ AND SET ACCORDINGLY THE VALUES)
POSSIBLE VALUES= --> 1 1 0 FOR XY
--> 1 0 1 FOR XZ
--> 0 1 1 FOR YZ
POSSIBLE VALUES= --> ANY VALUE
POSSIBLE VALUES= --> ANY VALUE
POSSIBLE VALUES= The value is defined as (Re=(RRES*UFREESTREAM*CHARLENGTH)/(VISC)),
and it is used to determing the freestream value of viscosity
POSSIBLE VALUES= --> ANY VALUE
POSSIBLE VALUES= 1 --> CENTRAL SCHEME NO LIMITER
2 --> MUSCL (DEFAULT)
3 --> WENO VARIANTS
POSSIBLE VALUES= 1 --> HLLC
2 --> RUSANOV(LLF)
3 --> ROE
4 --> HYBRID ROE-HLL (CARBUNCLE FREE)
POSSIBLE VALUES= 1,2,3,..,7 --> SPATIAL ORDER OF ACCURACY
USEFUL EVEN WHEN USING CENTRAL OR WENO LIMITERS, SINCE SOME CELLS MIGHT NOT HAVE SUFFICIENT NUMBER OF DIRECTIONAL STENCILS, OR DUE TO MOOD TECHNIQUE THEY MIGHT REVERT TO MUSCL METHOD
POSSIBLE VALUES= 1 --> MINMOD (BARTH AND JESPERSEN EQUIVALENT LIMITER)
2 --> MOG (MOG LIMITER)
3 --> MOGE
4 --> MOGV
5 --> VAN ALBADA
6 --> VAN LEER
7 --> VENKATAKRISHNAN
POSSIBLE VALUES= 1 --> GENERIC (DEFAULT x+y+z+x^2+y^2+z^2+xy+zy+xz)
2 --> LEGENDRE (SHIFTED FROM O TO 1)
POSSIBLE VALUES= 1 --> CONSERVED (DEFAULT)
2 --> CHARACTERISTICS(WORKS ONLY FOR WENO TYPE OF SCHEMES)
3 --> PRIMITIVE (SUITABLE FOR MULTICOMPONENT FLOWS)
POSSIBLE VALUES= 0 --> DEFAULT
1 --> RESTRICTIVE
2 --> SYMMETRICAL ONES
5 --> COMPACT WENO/WENOZ (YOU MUST USE THIS SETTING FOR
ACTIVATING COMPACT WENO/WENOZ SCHEMES)
APPLICABLE TO WENO METHOD ONLY
POSSIBLE VALUES= 0 --> DEFAULT (WHEN EES=5 IT ACTIVATES THE CWENO VARIANT)
1 --> CWENOZ WHEN EES=5
POSSIBLE VALUES= --> ANY VALUE
(USE 10^3-10^6 FOR CWENO (higher values more suitable for smooth problems, 10^5 works across many problems))
(USE 2-100 FOR CWENOZ)
(USE 100-10^5 FOR WENO)
POSSIBLE VALUES= 1 --> FORWARD EULER (CFL LIMIT <1.0)
2 --> 2ND-ORDER RUNGE-KUTTA (SSP) (CFL LIMIT <1.0)
3 --> 3RD-ORDER RUNGE-KUTTA (SSP) (CFL LIMIT <1.0)
4 --> 4TH-ORDER RUNGE-KUTTA (SSP) (CFL LIMIT <1.5)
5 --> FORWARD EULER WITH LOCAL TIME STEPPING FOR STEADY STATE PROBLEMS (CFL LIMIT <1.0)
10 --> IMPLICIT BDF-EULER FOR STEADY STATE PROBLEMS (NO CFL LIMIT)
11 --> IMPLICIT DUAL TIME STEPPING SECOND ORDER FOR UNSTEADY PROBLEMS (NO CFL LIMIT)
12 --> EXPLICIT DUAL TIME STEPPING SECOND ORDER FOR UNSTEADY PROBLEMS (CFL LIMIT <1.0)
POSSIBLE VALUES= --> ANY VALUE (ACCORDING TO THE TEMPORAL DISCRETISATION METHOD)
FOR DUAL TIME STEPPING PROBLEMS THE CFL NUMBER CORRESPONDS ONLY TO THE
CFL NUMBER USED FOR THE PSEUDO STEADY-STATE PROBLEM AT EACH NEWTON ITERATION
(HENCE A LARGE VALUE SHOULD BE ASSIGNED FOR OPTION 10,11 TO ACCELERATE CONVERGENCE)
POSSIBLE VALUES= --> ANY VALUE
USED ONLY BY OPTION (11,12) DUAL TIME STEPPING FOR ADVANCING THE SOLUTION.
UPPER LIMIT OF ITERATIONS FOR PSEUDO-STEADY STATE PART OF DUAL-TIME STEPPING
POSSIBLE VALUES= --> ANY VALUE (FOR OPTION 12 A VALUE OF 20 IS MORE THAN ENOUGH FOR
CONVERGENCE TO THREE ORDERS OF MAGNITUDE REDUCTION IN RESIDUAL)
IF THIS NUMBER OF ITERATIONS IS NOT SUFFICIENT THE DUAL TIME WILL PROCEED TO THE
NEXT STEP
NORMALISED RESIDUAL CONVERGENCE CRITERION FOR STEADY STATE PROBLEMS (OR PSEUDO-STEADY STATE COMPONENT OF DTS)
POSSIBLE VALUES= --> ANY VALUE (FOR OPTION 11, 12 A VALUE OF 0.001) IS MORE THAN ENOUGH FOR
A WIDE RANGE OF PROBLEMS
FOR OPTION (5, 10) A VALUE CLOSE TO 0.00001 MIGHT BE REQUIRED
PRESENCE OF PERIDIC BOUNDARY IN THE DOMAIN
POSSIBLE VALUES= 1 --> PERIODIC
0 --> NON PERIODIC
POSSIBLE VALUES= 0 --> SUPERSONIC
1 --> SUBSONIC (BY DEFAULT FARFIELD IS DETERMINED AUTOMATICALLY WITHIN THE CODE)
POSSIBLE VALUES= --> ANY VALUE (DIVIDES THE GRID COORDINATES BY THE SCALER VALUE)
POSSIBLE VALUES= 0 --> LSQ (DEFAULT, EVERYTHING IS COMPUTED USING LSQ EXCEPT BAD QUALITY CELLS THAT USE GREEN GAUSS
ONLY FOR THE APPROXIMATION OF THE GRADIENTS FOR THE DIFFUSION FLUXES)
1 --> GREEN GAUSS (GREEN GAUSS ONLY FOR THE APPROXIMATION OF THE GRADIENTS FOR THE DIFFUSION FLUXES)
POSSIBLE VALUES= 0 --> NO CORRECTION
1 --> LMACH CORRECTION (IMPROVES MAINLY THE LOW-ORDER MUSCL AND WENO SCHEMES UP TO 3RD-ORDER, ARTIFACTS
MAY APPEAR WHEN ENGAGED WITH HIGHER-ORDER METHODS)
POSSIBLE VALUES= --> ANY VALUE
POSSIBLE VALUES= --> ANY VALUE
A CHECKPOINT FILE AND OUTPUT FILE WILL BE WRITTEN WHEN THIS TIME IS MET
POSSIBLE VALUES= --> ANY VALUE
POSSIBLE VALUES= 1 --> TECPLOT BINARY (ONE FILE FOR THE ENTIRE DOMAIN)
2 --> VTK BINARY (ONE FILE FOR THE ENTIRE DOMAIN)
3 --> VTK BINARY PARTITIONED OUTPUT
4 --> TECPLOT BINARY PARTITIONED OUTPUT
HOW OFTEN (WALLCLOCK TIME IN SECONDS) TO WRITE AN OUTPUT FILE
POSSIBLE VALUES= --> ANY VALUE
HOW OFTEN (WALLCLOCK TIME IN SECONDS) TO WRITE A RESTART/CHECKPOINT FILE
POSSIBLE VALUES= --> ANY VALUE
HOW OFTEN (WALLCLOCK TIME IN SECONDS) TO WRITE AN AVERAGED OUTPUT FILE
POSSIBLE VALUES= --> ANY VALUE
ENABLE WRITING OF THE OUTPUT FILES FOR THE STENCILS FOR EACH OF THE PROBE LOCATIONS
POSSIBLE VALUES= 1 --> ENABLED
0 --> DISABLED
POSSIBLE VALUES= 1 --> ACTIVATED (SHOULD ONLY BE USED FOR UNSTEADY ILES, DDES,DES,URANS SIMULATIONS)
0 --> DEACTIVATED (DEFAULT)
ENABLE WRITING SURFACE OUTPUT SOLUTION FOR WALL BOUNDARIES
POSSIBLE VALUES= 1 --> ACTIVE
0 --> DEACTIVATED
POSSIBLE VALUES= 1 --> ACTIVE
0 --> DEACTIVATED
ENABLE WRITING SHEAR STRESSES ON SURFACE OUTPUT SOLUTION FOR WALL BOUNDARIES
POSSIBLE VALUES= 1 --> ACTIVE
0 --> DEACTIVATED
POSSIBLE VALUES= 0 --> WITHOUT TURBULENCE MODEL
1 --> WITH TURBULENCE MODEL
POSSIBLE VALUES= 0 --> STEADY
1 --> UNSTEADY
POSSIBLE VALUES= 0 --> NO PREVIOUS PASSIVE SCALAR
1 --> PREVIOUS PASSIVE SCALAR PRESENT IN RESTART FILE
POSSIBLE VALUES= 0 --> NO PREVIOUS TURBULENCE MODEL
1 --> SPALART-ALLMARAS
2 --> K-OMEGA
POSSIBLE VALUES= ANY VALUE --> ENSURE THAT YOU PROVIDE THEIR COORDINATES BELOW