#
# naca64 2D - Navier-Stokes
# Steady, Subsonic
#


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 BOUNDARY MAPPING
 ----------------------------------------------------- 
                    Markers: 1
                      Type : symmetry plane
 block end
 ---------------------------  
                    Markers: 2
                      Type : symmetry plane
 block end
 ---------------------------  
                    Markers: 3
                       Type: viscous wall
                   Subtype : laminar 
   Write surface data (0/1): 1 
       Monitor forces (0/1): 1
 block end
 ---------------------------  
                    Markers: 4
                       Type: viscous wall 
                   Subtype : turbulent 
   Write surface data (0/1): 1 
       Monitor forces (0/1): 1
 block end
 ---------------------------  
                    Markers: 5 
                      Type : farfield
   Write surface data (0/1): 1
       Angle alpha (degree): 0
        Angle beta (degree): 0
    Vortex correction (0/1): 0
               Chord length: 1
 block end
 ---------------------------  
 ----------------------------------------------------- 
 Required Parameters
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                            Boundary mapping filename: (thisfile)
                                Primary grid filename: NACA64A010.grid
                                           Grid scale: 1.0
                                Reference Mach number: 0.3

 ----------------------------------------------------- 
 IO
 ----------------------------------------------------- 
                                          Grid prefix: dualgrid
                                  Output files prefix: solution
                     Automatic parameter update (0/1): 1

 ----------------------------------------------------- 
 PREPROCESSING
 ----------------------------------------------------- 
                           Number of multigrid levels: 5

                Cache-coloring (0/max_faces in color): 200000
                                  Point fusing reward: 1.2
                           Structured grid coarsening: 0
                           Sharp edge angle (degrees): 0
                                         Output level: 10
                         Compute/store wall distances: 50

    Partitioning ------------------------------------: -
                                    Number of domains: 1
                          Type of partitioning (name): private
    Additionals -------------------------------------: -
                   2D offset vector (0 / x=1,y=2,z=3): 2
 

 ----------------------------------------------------- 
 SOLVER
 ----------------------------------------------------- 
    Timestepping Start/Stop -------------------------: -
                                        Output period: 999999
                             Maximal time step number: 200
    Geometry ----------------------------------------: -
                              Reference relation area: 0
                 Reference length (pitching momentum): 1
           Reference length (rolling/yawing momentum): 1
                                  Origin coordinate x: 0.25
                                  Origin coordinate y: 0
                                  Origin coordinate z: 0
    Monitoring --------------------------------------: -
                                Monitor history (0/1): 1
                                    Monitoring values: Residual_C-lift_C-drag_C-my_Fx_Fz_My_Angle-a
    Transport coefficients --------------------------: -
                                      Reynolds number: 7500000
    Flux --------------------------------------------: -
             Convective RANS flux discretization type: upwind
                     Viscous flux type TSL/Full (0/1): 1
                          Reconstruction of gradients: Green_Gauss
                Riemann solver for first order scheme: Van_Leer
               Riemann solver for second order scheme: AUSMDV
                       Order of basic equations (1/2): 2
                  Order of additional equations (1/2): 1
    Multigrid ---------------------------------------: -
                              MG description filename: 4w
    Timestepsize ------------------------------------: -
                                           CFL number: 1.8
                            CFL number (coarse grids): 3.06
                            CFL number (large grad p): 1.8
    Turbulence --------------------------------------: -
                               Ratio Prandtl lam/turb: 0.8
                            General ratio mue-t/mue-l: 0.1
                            Maximum limit mue-t/mue-l: 20000
                          General turbulent intensity: 0.001
                               Reference bl-thickness: 1e+22
                             Turbulence model version: SAE
             Turbulence equations use multigrid (0/1): 1
            Maximum turbulence production/destruction: 1000
                  Omega boundary condition type (0/1): 0
                    Boussinesq mod. for K-Omega (0/1): 0
                                  K-omega wall factor: 10
                      Kato Launder modification (0/1): 0
                              K-omega limitation type: standard
                                            Minimum k: 1e-05
                                        Minimum omega: 1e-05
                                    Positivity scheme: 0
                                EARSM expansion order: 1
                       Vortical flow correction (0/1): 0
        Turbulence diffusion flux type TSL/Full (0/1): 1

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 Updates
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