t pa -----------------------------------------------------
 Boundary mapping filename: (thisfile)
 -----------------------------------------------------
 BOUNDARY MAPPING
 -----------------------------------------------------

            Markers: 12
                       Type: farfield
                       Name: farfield
       Angle alpha (degree): 7.0
                Mach number: 0.15
 block end
 ---------------------------

            Markers: 2
                       Type: viscous wall
                    Subtype: transition
                       Name: airfoil_lower
   Write surface data (0/1): 1
       Monitor forces (0/1): 1
 block end
            Markers: 22
                       Type: viscous wall
                    Subtype: transition
                       Name: airfoil_upper
   Write surface data (0/1): 1
       Monitor forces (0/1): 1
 block end 
---------------------------

            Markers: 230
               Type: symmetry plane
               Name: Side1
 block end
 ---------------------------

            Markers: 231
               Type: symmetry plane
               Name: Side2
 block end


 -----------------------------------------------------
 TRANSITION DATA INPUT
 -----------------------------------------------------

Boundary part namelist: airfoil_upper
         Number of polyline points: 1
                    Laminar height: 30

TransitionCoordinates
0.42  0.0  0.129881
transition end
 ---------------------------

Boundary part namelist: airfoil_lower
         Number of polyline points: 1
                    Laminar height: 30

TransitionCoordinates
0.3  0.0  -0.0301982
transition end
 ---------------------------

 -----------------------------------------------------
 Cut plane output
 -----------------------------------------------------
   Plane output description file: (thisfile)
        Plane output period: 999999
	Plane output values: xyz_rho_cp_yplus_cf_cfsgnx_cfxyz_bldata
           Number of planes: 1
   Boundary type (euler/ns): ns
            Plane support x: 0.
            Plane support y: 0.0
            Plane support z: 0.
             Plane normal x: 0.
             Plane normal y: 1.
             Plane normal z: 0.

 -----------------------------------------------------
 Surface output
 -----------------------------------------------------
   Surface output description file: (thisfile)
     Surface output files prefix: surface_output
           Surface output values: xyz_rho_cp_vx_vy_vz_mach_yplus_cf_cfsgnx_cfxyz_h12_delta_theta_dstar ###############
           Surface output period: 999999

 -----------------------------------------------------
 Extra field pointdata output
 -----------------------------------------------------
   Field output description file: (thisfile)
   Field output values: cp_mach_Rrho_Rvx_Rvy_Rvz_vort_wdist
 
 -----------------------------------------------------
 IO
 -----------------------------------------------------
    Files/IO ----------------------------------------: -
                                Primary grid filename: AS-B.airfoil_netcdf_2sides
                                          Grid prefix: ../../Dualgrid.TR/AS-B.airfoil_netcdf_2sides.dualgrid
                                  Output files prefix: solution.g++_LUSGS.6
                               #Detailed output (0/1): 1 -> new: > 50->first debug-level, > 100->full debug information
                                         Output level: 60

                     Automatic parameter update (0/1): 1
		          Accumulate queue time (0/1): 1
                  Write pointdata dimensionless (0/1): 1
    Solver ------------------------------------------: -
                              MG description filename: 4w
                                  Monitoring filename: my-monitor-list
 -----------------------------------------------------
 PREPROCESSING
 -----------------------------------------------------
                Cache-coloring (0/max_faces in color): 50000
                         Compute/store wall distances: 1

                                    Number of domains: 1
                          Type of partitioning (name): private
            
                          Compute lusgs mapping (0/1): 1

                   2D offset vector (0 / x=1,y=2,z=3): 2

      Maximum wall distance for points on wall normal: 0.02

 -----------------------------------------------------
 ADAPTATION
 -----------------------------------------------------

                Change wall normal distribution (0/1): 1
                                Indicator0 Ht-scaling: 0
                                Indicator0 Pt-scaling: 0
                               Indicator0 rho-scaling: 0
                                 Indicator0 V-scaling: 0
                             Percentage of new points: 0
                       Maximum surface angle (degree): 30

 -----------------------------------------------------
 SOLVER
 -----------------------------------------------------
    Timestepping Start/Stop -------------------------: -
                                        Output period: 999999 2000
                             Maximal time step number: 12000
                                     Minimum residual: 1e-09
				                                  Matching period: 150
    Geometry ----------------------------------------: -
                                           Grid scale: 1.0
					   
#                             Reference relation area: 0 <- automatische Berechnung!    
			      Reference relation area: 1.0
                 Reference length (pitching momentum): 0
           Reference length (rolling/yawing momentum): 0
                                  Origin coordinate x: 0
                                  Origin coordinate y: 0
                                  Origin coordinate z: 0
    Dual time ---------------------------------------: -
                        #Unsteady calculation (0/1/2): 0 -> new: (none)->local-time, dual->dual-time, global->global-time
                               Unsteady time stepping: (none)
                Unsteady show pseudo time steps (0/1): 0
                     Unsteady physical time step size: 0.862
                         Unsteady physical time steps: 100
              Unsteady inner iterations per time step: 40
     Minimum number of inner iterations per time step: 0
              #Unsteady implicit scheme order (1/2/3): 2 -> new!
                       Unsteady implicit scheme order: 2
              #Unsteady extrapolation order (0/1/2/3): 1 -> new!
                         Unsteady extrapolation order: 1
                         Unsteady residual type (0/1): 1
    Monitoring --------------------------------------: -
                                Monitor history (0/1): 1
                       Residual monitoring type (0/1): 1
                                    Monitoring values: Residual_Max-res_dnue/dt_C-lift_C-drag_C-my_Max-y+_Max-eddyv
                       Monitoring significant figures: 4_4_4_4_4_4_4_4   
    Memory management -------------------------------: -
                                Increase memory (0/1): 1
    Variables ---------------------------------------: -
                            Fix negative values (0/1): 0
			              Minimal density: 1e-12
                                     Minimal pressure: 1e-12
                                       Minimal energy: 1e-12
    Flux/Solver/Dissipation -------------------------: -
                    #Solver type upwind/central (0/1): 1 0 -> new: central, upwind, mixed
             Convective RANS flux discretization type: central -> OLD name!
                   #Inviscid flux discretization type: Central
		     Hold static velocity field (0/1): 0
                                      #Central solver: Classic_dissipation -> new: Scalar_dissipation, Matrix_dissipation
                           Central dissipation scheme: Scalar_dissipation
		            Central solver k-w scheme: Roe
			    
                     #Central classic dissipation 2nd: 0.25 0.5 -> new!
                    2nd order dissipation coefficient: 0.5
             #Inverse central classic dissipation 4th: 64 -> new!
            Inverse 4th order dissipation coefficient: 64
	                  #Central matrix dissipation: 0.5 1 -> new!
                 Matrix dissipation terms coefficient: 0.5 1
    Minimum artificial dissipation for acoustic waves: 0.2
          Minimum artificial dissipation for velocity: 0.2
	                    
                          Reconstruction of gradients: Green_Gauss
                           #First order upwind solver: Van_Leer -> new!
                Riemann solver for first order scheme: Van_Leer
                          #Second order upwind solver: AUSMDV -> new!
               Riemann solver for second order scheme: AUSMDV
                       Order of basic equations (1/2): 2
                  Order of additional equations (1/2): 1
		  
                        Mach number limit for limiter: 0
                        Lowest pressure for 2nd order: 0
                        Use line reconstruction (0/1): 1
                               AUSMDV shock fix (0/1): 0
                                          AUSMP alpha: 0.1875
                                           AUSMP beta: 0.125
                                AUSMP pressure weight: 1
                              Ausm scheme dissipation: 0.25		       
    Limiter -----------------------------------------: -
                         Limiter freezing convergence: 3.0 0
		     Venkatakrishnan limiter constant: 0
    Flowfield initialization ------------------------: -
                          Init total conditions (0/1): 0		  		  
    Relaxation --------------------------------------: -
                                    Relaxation solver: Backward_Euler
    Runge Kutta -------------------------------------: -
                            #Number Runge-Kutta steps: 3
                         Number of Runge-Kutta stages: 3	    
    Backward Euler ----------------------------------: -
                                        Linear solver: Lusgs
                                Linear preconditioner: (none)
                        Implicit overrelaxation omega: 1
                         Implicit overrelaxation beta: 1
    LUSGS -------------------------------------------: -
                                   Sgs stages maximum: 3
         Lusgs increased parallel communication (0/1): 0
                   Lusgs treat whirl implicitly (0/1): 0	  		  
    Multigrid ---------------------------------------: -
                              MG description filename: 2v
                        SG start up steps (fine grid): 0
			        MG source terms (0/1): 0
                        Interpolate corrections (0/1): 0
			   Number of multigrid levels: 5
    Full multigrid ----------------------------------: -
                                Multigrid start level: 1
              Maximal time step number (coarse grids): 30 0
                      Minimum residual (coarse grids): 0.001
    Timestepsize ------------------------------------: -
                                           CFL number: 150.5
                            CFL number (coarse grids): -1
                            CFL number (large grad p): -1
                              Infinite timestep (0/1): 0
                             Project time steps (0/1): 1
                           Time step smoothing factor: 0
    Smoother ----------------------------------------: -
                                    Residual smoother: Point_explicit
                                  Correction smoother: Point_explicit
                            Correction smooth epsilon: 0.2    -1 
                              Residual smooth epsilon: 0.2002 -1 
                           Correction smoothing steps: 2
                             Residual smoothing steps: 2
                           Smoothing relaxation steps: 2
                       No smoothing near shocks (0/1): 0
    Preconditioning ---------------------------------: -
                              Preconditioning (0/1/2): 2
                                        Cut-off value: 1		       	       
    Perfect gas thermodynamic -----------------------: -
                                       Gas constant R: 287.053

                                   Gas constant gamma: 1.4	       	       
    Transport coefficients --------------------------: -
                                      Reynolds number: 2.0E+06
				      
				       Prandtl number: 0.72
                                  Sutherland constant: 110.4
                       Sutherland reference viscosity: 1.716e-05
                     Sutherland reference temperature: 273
    References --------------------------------------: -
##				    Reference density: 1.29250880647192
                                Reference temperature: 285.00
##                                 Reference pressure: 101325
				
                                      Reynolds length: 1.0
                                Reference Mach number: 0.15

                             Reference outer pressure: 101325
##                                                     !!!!!!
## -> WATCH OUT for internal flows and configurations with open contours, e.g. half bodies!			     		
    Turbulence --------------------------------------: -
                               Ratio Prandtl lam/turb: 0.8
                                    Ratio mue-t/mue-l: 0.1
                            Maximum limit mue-t/mue-l: 20000
                                  Turbulent intensity: 0.001
                               Reference bl-thickness: 1e+22
                                                    # -> new: SAE, Wilcox_k-w, RSM
                             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 -> new!
                                  K-omega wall factor: 10
                      Kato Launder modification (0/1): 0
                     #K-omega limitation type (0/1/2): 0 -> new: standard, Rudnik, Schwarz
                              K-omega limitation type: standard
                                            Minimum k: 1e-05
                                        Minimum omega: 1e-05
                                    Positivity scheme: 0
                     #EARSM expansion order (1/2/3/4): 1 -> as before: 1, 2, 3, 4
                                EARSM expansion order: 1
                       Vortical flow correction (0/1): 0
      IO ----------------------------------------------: -
                    Write pointdata dimensionless (0/1): 0
    Reference system of forces and moments (tau/ln9300): tau
 =====================================================
 Transition Prediction
                            Transition prediction (0/1): 0 1
#                                    TM fast test (0-2): 2 0 -> Available only for Krimmelbein!
	         Transition prediction description file: (thisfile)										
                                Info output level (0-5): 5																																
                                File output level (0/1): 1
                          File output in pre-mode (0/1): 0
		    Max. number of points on wallnormal: 128
                    Min. number of points on wallnormal: 128
	                  Max. distance for wallnormals: 1e+20
	         Lim. angle to detect sharp edges (deg): 30
		                       Integration mode: 0
	            Write streamline data to file (0/1): 1   
	    Write boundary layer profiles to file (0/1): 1
                            Streamline integration mode: 0
#                                                      Not yet used!    
                            Profiles interpolation mode: 0
#                                                      Not yet used!
	                          Smooth pressure (0/1): 0
               --------------------------------------
                             Defaults TransitionBlock

                        Prediction start iteration nr: 1000
                          Prediction end iteration nr: 20500
                                    Prediction period: 1000
                --------------------------------------
                        TS transition prediction mode: 10
                        CF transition prediction mode: 0
                       LSB transition prediction mode: 0
                       ALT transition prediction mode: 0 
#               			      Mode  9: Database Methods
#                    		              Mode 10: Linear Stability Code LILO

                             Boundary layer data mode: 0
#             	 			      Mode  0: use TAU  BL-data for transition prediction
#  	     			     	      Mode  1: use COCO BL-data for transition prediction
#  		       			      Mode  2: use COCO for CF, use TAU for TS
#		       			      Mode  3: use COCO for TS, use TAU for CF

                                 Critical N-factor TS: 9.0
                                 Critical N-factor CF: 4.0
                           N-ts/N-cf Diagram (points): 0 3
                             N-ts/N-cf Diagram (N-TS):  6.50  6.50  0.00
                             N-ts/N-cf Diagram (N-CF):  0.00  5.50  5.50

                   Offset for polylines extrapolation: 0.5 1.0

                                    Relaxation factor: 0.6
                         Maximum delta for transition: 0.1

              Minimum N-factor for extrapolation (TS): 0.001
              Minimum N-factor for extrapolation (CF): 0.001

                --------------------------------------
#               Mode 1: transition at cp,min + offset -> offset = "Pre-Maximum delta for transition"
#               Mode 2: laminar separation from TAU
#               Mode 3: laminar separation from Coco (NOT YET AVAILABLE!)

                                  Pre-prediction mode: 2
                    Pre-prediction start iteration nr: 20
                      Pre-prediction end iteration nr: 1000
                                Pre-prediction period: 20
                                Pre-relaxation factor: 1.0
                     Pre-maximum delta for transition: 1000.0
                            Offset for pmin criterion: 0

                                  TransitionBlock end
               ======================================    
                                      TransitionBlock

                                   Boundary part list: airfoil_upper
                                Transition block name: airfoil_upper
				
#		Type 1: Inviscid streamline, integrated from boundary layer edge velocity
#		Type 2: Streamline parallel to oncoming flow
#		Type 3: Attachment line	
                                      Streamline type: 2

                         Maximum delta for transition: 0.005

                          Number of streamline points: 0
#			  3D: Number of start coordinates for streamline calculation

                            Number of limiting planes: 0
#			  3D: Streamline calculation stops, if streamline cuts one of limiting planes			    
                       
                                  TransitionBlock end
               --------------------------------------
                                      TransitionBlock

                                   Boundary part list: airfoil_lower
                                Transition block name: airfoil_lower
                                      Streamline type: 2

                          Number of streamline points: 0

                            Number of limiting planes: 0


 
	                              Coco input parameter:
	                              --------------------
                                      Coco executable: ./tm_BLcode_coco
                            Keep Coco log files (0/1): 1
                            Keep Coco run files (0/1): 1
                       Keep Coco profiles files (0/1): 0

                                    Prepcp input parameter:
                                    ----------------------
                                    Prepcp executable: ./tm_CPtool_prepcp
                              Keep Prepcp files (0/1): 1
                                   Use Prepcp (0/1/2): 0
#                            0: Prepcp is not used
#                            1: Prepcp is used to determine effective sweep angle
#                            2: Prepcp is used to modify cp-distribution
                 Prepcp factor for number of stations: 1.0
#                            Factor to increase number of streamline stations in Prepcp

	                              Lilo input parameter:
	                              --------------------
                                      Lilo executable: ./tm_STABcode_lilo
                            Keep Lilo log files (0/1): 1
                            Keep Lilo run files (0/1): 1

  	      Number of frequencies/wave lengths NWAV: 40

	                               Database methods input parameter:
	                               -------------------------------- 
                                       Dbm executable: ./tm_eN_DatabaseModule 
                             Keep Dbm run files (0/1): 1
																													
                       Number of TS frequencies NF_TS: 60
             TS analysis incomp./comp. NCOMP_TS (0/1): 0	
                   Coupling via cf/h,in NHIN_TS (0/1): 1
																				
                       Number of CF frequencies NF_CF: 100
                             Initial frequency FRINIT: 0.12e5
            Decreasing logarithmic frequency step DFR: -0.84319e-1
             CF analysis incomp./comp. NCOMP_CF (0/1): 0
                  Number of different psi values NPSI: 30
                   Initial value of psi (deg) PSIINIT: 89.9
                       Decreasing psi step (deg) DPSI: 1.0
                        
 =======================================================================   
 -----------------------------------------------------------------------
 Updates
 -----------------------------------------------------------------------

   

    

    solver at Thu Sep 13 19:23:19 2007
                                  Restart-data prefix: solution.g++_LUSGS.6.pval.7691 
    solver at Thu Sep 13 19:23:19 2007
                              Surface output filename: solution.g++_LUSGS.6.surface.pval.7691 

    solver at Fri Sep 14 14:51:39 2007
                                  Restart-data prefix: solution.g++_LUSGS.6.pval.12720 
    solver at Fri Sep 14 14:51:39 2007
                              Surface output filename: solution.g++_LUSGS.6.surface.pval.12720 