#
# naca0012 2D - Euler
# Steady, Transonic
# Mach number    : 0.755
# Angle of attack: 2 degrees
#

 -----------------------------------------------------
 BOUNDARY MAPPING
 -----------------------------------------------------


                      Type : farfield
                    Markers: 4
       Angle alpha (degree): 2.0
 block end
 ---------------------------  
                      Type : euler wall
                    Markers: 5
 block end
 ---------------------------  
                      Type : symmetry plane
                    Markers: 1
 block end
 ---------------------------  
                      Type : symmetry plane
                    Markers: 2
 block end
 ---------------------------  
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 Required Parameters
 ----------------------------------------------------- 
                            Boundary mapping filename: (thisfile)  
                                Primary grid filename: naca0012.grid
                                           Grid scale: 1.0
                                Reference Mach number: 0.755
                                       
 ----------------------------------------------------- 
 IO
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                                          Grid prefix: dualgrid
                                  Output files prefix: solution
    Solver ------------------------------------------: -
                     Automatic parameter update (0/1): 1
                  Write pointdata dimensionless (0/1): 0

 ----------------------------------------------------- 
 PREPROCESSING
 -----------------------------------------------------
                                    Number of domains: 1
  
    Runtime optimisation ----------------------------: -
                Cache-coloring (0/max_faces in color): 200000
                   2D offset vector (0 / x=1,y=2,z=3): 2

 ----------------------------------------------------- 
 SOLVER
 ----------------------------------------------------- 
             Convective RANS flux discretization type: central
                           Central dissipation scheme: Scalar_dissipation

    Timestepping Start/Stop -------------------------: -
                                        Output period: 999999
                             Maximal time step number: 200

                         Number of Runge-Kutta stages: 3
                                           CFL number: 1.8

    MG-----------------------------------------------: -
                              MG description filename: 4w
                            CFL number (coarse grids): 3.0 

    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
 -----------------------------------------------------
 Extra field pointdata output
 -----------------------------------------------------
  Field output description file: (thisfile)
  Field output values: cp_mach


 ----------------------------------------------------- 
 Updates
 ----------------------------------------------------- 

                                  Restart-data prefix:

