#
# delta wing, 3D - Euler
# Steady, Transonic
#
 -----------------------------------------------------
 BOUNDARY MAPPING
 -----------------------------------------------------
                            Boundary mapping filename: (thisfile)
-----------------------------------------------------
                                                  Type: farfield
                                               Subtype: (none)
                                               Markers: 17-18
                                                  Name: Farfield
                                  Angle alpha (degree): 9.0
                                             block end
-----------------------------------------------------
                                                  Type: euler wall
                                               Subtype: (none)
                                               Markers: 1
                                                  Name: Fuselage_Right_Top
                              Write surface data (0/1): 1                   
                                             block end
-----------------------------------------------------
                                                  Type: euler wall
                                               Subtype: (none)
                                               Markers: 2
                                                  Name: Right_Wing_Top
                              Write surface data (0/1): 1                   
                                             block end
-----------------------------------------------------
                                                  Type: euler wall
                                               Subtype: (none)
                                               Markers: 3
                                                  Name: Right_Wing_Bot
                              Write surface data (0/1): 1                   
                                             block end
-----------------------------------------------------
                                                  Type: euler wall
                                               Subtype: (none)
                                               Markers: 4
                                                  Name: Fuselage_Right_Bot
                              Write surface data (0/1): 1                   
                                             block end
-----------------------------------------------------
                                                  Type: euler wall
                                               Subtype: (none)
                                               Markers: 7
                                                  Name: Fuselage_Left_Top
                              Write surface data (0/1): 1                   
                                             block end
-----------------------------------------------------
                                                  Type: euler wall
                                               Subtype: (none)
                                               Markers: 8
                                                  Name: Left_Wing_Top
                              Write surface data (0/1): 1                   
                                             block end
-----------------------------------------------------
                                                  Type: euler wall
                                               Subtype: (none)
                                               Markers: 9
                                                  Name: Left_Wing_Bot
                              Write surface data (0/1): 1                   
                                             block end
-----------------------------------------------------
                                                  Type: euler wall
                                               Subtype: (none)
                                               Markers: 10
                                                  Name: Fuselage_Left_Bot
                              Write surface data (0/1): 1                   
                                             block end
-----------------------------------------------------
                                                  Type: euler wall
                                               Subtype: (none)
                                               Markers: 5-6,11-16
                                                  Name: Sting
                              Write surface data (0/1): 1
                                             block end
 -----------------------------------------------------
 ----------------------------------------------------- 
 Required Parameters
 ----------------------------------------------------- 
                            Boundary mapping filename: (thisfile)
                                Primary grid filename: Mesh/delta_euler.grid
                                           Grid scale: 1


 ----------------------------------------------------- 
 IO
 ----------------------------------------------------- 

    Grid/Solution -----------------------------------: -
                                          Grid prefix: Mesh/dualgrid
                                  Output files prefix: Results/delta_euler

 -----------------------------------------------------
 PREPROCESSING
 -----------------------------------------------------
    Parameter ---------------------------------------: -
                           Number of multigrid levels: 1
                                         Output level: 5
    Runtime optimisation ----------------------------: -
                Cache-coloring (0/max_faces in color): 200000
                         Bandwidth optimisation (0/1): 0
                   2D offset vector (0 / x=1,y=2,z=3): 0
    Partitioning ------------------------------------: -
                                    Number of domains: 1
                       Number of primary grid domains: 1
                                    Smooth partitions: 0
                          Type of partitioning (name): private


 ----------------------------------------------------- 
 SOLVER
 ----------------------------------------------------- 
    Files/IO ----------------------------------------: -
                                  Restart-data prefix: (none)
                                  Output files prefix: Results/delta_euler
                      Profile output description file: (none)
                        Plane output description file: (none)
                      Surface output description file: (thisfile)
                        Field output description file: (thisfile)
                                                     : -
                     Automatic parameter update (0/1): 1
                          Accumulate queue time (0/1): 0
    Timestepping Start/Stop -------------------------: -
                                        Output period: 99999
                             Maximal time step number: 50
                                     Minimum residual: 1.e-6
                                      Matching period: 150
    Memory management -------------------------------: -
                                Increase memory (0/1): 1
    Perfect gas thermodynamic -----------------------: -
                                       Gas constant R: 287
                                   Gas constant gamma: 1.4
    Transport coefficients --------------------------: -
                            Viscous calculation (0/1): 0
                                      Reynolds number: 3684300
    Geometry ----------------------------------------: -
                                           Grid scale: 1
                              Reference relation area: 0.1061
                 Reference length (pitching momentum): 0.4819
           Reference length (rolling/yawing momentum): 0.1914
                                  Origin coordinate x: 0
                                  Origin coordinate y: 0
                                  Origin coordinate z: 0
    References --------------------------------------: -
                                Reference temperature: 305.36
                                   Reference pressure: 67494
                                      Reynolds length: 0.4819
                                Reference Mach number: 0.5
    Variables ---------------------------------------: -
                            Fix negative values (0/1): 0
                                      Minimal density: 1e-12
                                     Minimal pressure: 1e-12
                                       Minimal energy: 1e-12
    Flux --------------------------------------------: -
             Convective RANS flux discretization type: central
                           Central dissipation scheme: Scalar_dissipation
                            Central solver k-w scheme: Roe
                    2nd order dissipation coefficient: 0.5
            Inverse 4th order dissipation coefficient: 64
                          Reconstruction of gradients: Green_Gauss
    Flowfield initialization ------------------------: -
                          Init total conditions (0/1): 0
    Multigrid ---------------------------------------: -
                              MG description filename: sg
                        SG start up steps (fine grid): 0
                                MG source terms (0/1): 0
    Monitoring --------------------------------------: -
                                Monitor history (0/1): 0
                                    Monitoring values: Residual_C-lift_C-drag_C-my_Fx_Fz_My_Angle-a
 -----------------------------------------------------
                       Automatic parameter update (0/1): 1

 -----------------------------------------------------
 Extra field pointdata output
 -----------------------------------------------------
  Field output description file: (thisfile)
  Field output values: cp_mach
  Output period: 99999

  Surface output description file: (thisfile)
  Surface output values: cp_fxyz_mach
  Surface output period: 99999

 -----------------------------------------------------
 AMIF settings for tau2plt
 -----------------------------------------------------
                                         Output format: amif
               Create surface zone for boundary marker: 1,2,3,4,5,6,7,8,9,10,11,12,13,14,15,16
                                  Title of output file: DELTA


 -----------------------------------------------------
 Settings for Deformation
 -----------------------------------------------------
    External deformation --------------------------: -
                      Deformed coordinates filename: Shape/delta_surf.ami
              Use coordinates as displacement (0/1): 0
                       Deformation reduction factor: 1
     Grid smoothing -------------------------------: -
              Smoothing iterations for inner tetras: 0
               Smoothing selection angle for tetras: 0
                        Smoothing relaxation factor: -1

 -----------------------------------------------------

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