#
# naca0012 2D - Euler
# Unsteady, Transonic
# Pitching oscillation
#

 -----------------------------------------------------
 BOUNDARY MAPPING
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                      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
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                            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: pitch
    Solver ------------------------------------------: -
                     Automatic parameter update (0/1): 1
                  Write pointdata dimensionless (0/1): 0

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

    Timestepping Start/Stop -------------------------: -
                                        Output period: 25
                             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
    Dual time ---------------------------------------: -
                               Unsteady time stepping: dual
                       Unsteady implicit scheme order: 2
                Unsteady show pseudo time steps (0/1): 1
     Minimum number of inner iterations per time step: 5
              Unsteady inner iterations per time step: 50
                         Unsteady physical time steps: 150
                         Unsteady extrapolation order: 1
    Grid movement -----------------------------------: -
                                Type of grid movement: rigid
                            Motion hierarchy filename: (thisfile)
                          Motion description filename: (thisfile)
                         ----------------------------: -
                                            Node name: aircraft
                                 Node reference frame: inertial
                             Node controls grid block: 1
                           Node motion description id: aircraft
                                              hdf end
                         ----------------------------: -
                      Number of time steps per period: 50
                  Evaluate forces and moments at node: aircraft
                         ----------------------------: -
                                Motion description id: aircraft
                                     Type of movement: periodic
                    Origin of local coordinate system: 0.25 0.0 0.0
                Degree of Fourier series for rotation: 1
                       Reduced frequency for rotation: 0 0.1628 0
                   Reduced frequency reference length: 1.0 1.0 1.0
        Fourier coefficients for rotation (sin) pitch: 0.0 2.51
                                              mdf end

    Monitoring --------------------------------------: -
                                Monitor history (0/1): 1
                                    Monitoring values: Residual_C-lift_C-drag_C-my_Fx_Fz_My_Angle-a_T/tperiod

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


 -----------------------------------------------------
 Steady restart conditions
 -----------------------------------------------------
    solver at Tue Mar 21 07:16:48 2006
                                  Restart-data prefix: solution.pval.200 

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