DefaultCaseFile.HiOCase

!
!       ////////////////////////////
! 	    // Default parameter file //
!	   ////////////////////////////
!

!-------------------------------------: Geometry
                             Mesh file: ./MESH/*.HiOMesh
                         Boundary file: _this_

!-------------------------------------: Physics
                Gas                   : Air
                Reference pressure    : 101325.0
                Reference Temperature : 273.15
                Reynolds length       : 1.0
                Reynolds number       : 1000.0
                Prandtl number        : 0.72
                Mach number           : 0.1
	
!------------------------------------: DG Discretization
                 Interpolation nodes : Legendre-Gauss
         Default polynomial order    : 8

!------------------------------------: Initialization
                   Initial condition : Uniform
                   Restart file      : ./RESULTS/*.HiORst

!------------------------------------: Inviscid discretization
             Inviscid discretization : Standard
               Inviscid formulation  : Green form
             Inviscid Riemann solver : Roe            ! HLL 

!------------------------------------: Viscous discretization
               Viscous discretization: BR1            ! IP
              Interior penalty method: IIPG           ! NIPG/SIPG/IIPG
              Jumps penalty parameter: 1.0
     Gradient jumps penalty parameter: 0.0

!------------------------------------: Artificial dissipation
         Artificial dissipation (0/1): 0
         Artificial dissipation type: Laplacian          ! Physical
         Artificial dissipation indicator: Jumps-based
         Artificial dissipation intensity: 0.4

!-----------------------------------: Time integration
               Integration mode     : Steady             ! Transient
               Integration scheme   : Williamson RK5     ! Williamson RK3, Explicit-Euler
               Time step            : 1.0e-2
               CFL Number           : 0.4
               Simulation time      : 1.0
               Residual target      : 1.0e-5
               Number of iterations : 2000
               Initial time         : 0.0

!----------------------------------: Output variables
                      Solution file: ./RESULTS/*.HiORst
                  Autosave interval: 1000
                     Export format : Tecplot
                    Output interval: 10
                   Output file type: Interpolated
    Number of representation points: 10
                     Save variables: rho_rhou_rhov_rhoe_u_v_p_Mach_vort_rhot_rhout_rhovt_rhoet_muart

!
!       ///////////////////////////////////
! 	    // Default boundary mapping file //
!	   ///////////////////////////////////
!

# define p-Refinement
   zoneID: value
# end

# define zone i
   Name = Euler wall
   Type = Euler wall
# end 

# define zone i
   Name = Periodic
   Direction = x
   Marker = #2
# end 

# define zone i
   Name = Dirichlet / Farfield / Pressure inlet / Riemann
   Type = Dirichlet / Farfield / Pressure inlet / Riemann
   pressure = 
   Temperature =
   Mach = 
   Angle of attack
   Use function = 
# end

# define zone i
   Name = Pressure outlet
   Type = Pressure outlet
   pressure = 
   Temperature = 
   Mach = 
   Angle of attack = 
   Outflow type = Reflective / Partially non reflective
   Use function =
# end

# define zone i
   Name = newDirichlet
   Type = newDirichlet
   pressure = 
   Temperature = 
   Mach =
   Angle of attack = 
   Outflow pressure = Static / Total
   Mode = Specify speed / Specify total pressure
# end

# define zone i 
   Name = Viscous wall
   Type = Viscous wall
   Wall type = Adiabatic / Isothermal
   Wall temperature = 
   Mach number = 
   Velocity direction = [1.0 , 0.0]
# end

# define probe i
   Name = probe
   x position = 0.0
   y position = 0.0
   Variable = p
# end

# define surface monitor 1
   Name = lift
   Marker = 
   Variable = lift
   Reference surface = 1.0
# end

# define surface monitor 2
   Name = drag
   Marker = 5
   Variable = drag
   Reference surface = 1.0
# end