@@ -119,6 +119,15 @@ CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
119119%Navier-Stokes wall boundary marker(s) (NONE = no marker)
120120MARKER_HEATFLUX = (BLADE1, 0.0, BLADE2, 0.0, BLADE3, 0.0, HUB1, 0.0, SHROUD1, 0.0, HUB2, 0.0, SHROUD2, 0.0, HUB3, 0.0, SHROUD3, 0.0)
121121%
122+ % ------------------------ WALL FUNCTION DEFINITION --------------------------%
123+ %
124+ MARKER_WALL_FUNCTIONS = ( BLADE1, STANDARD_WALL_FUNCTION , BLADE2, STANDARD_WALL_FUNCTION , BLADE3, STANDARD_WALL_FUNCTION , HUB1, STANDARD_WALL_FUNCTION , SHROUD1, STANDARD_WALL_FUNCTION , HUB2, STANDARD_WALL_FUNCTION , SHROUD2, STANDARD_WALL_FUNCTION , HUB3, STANDARD_WALL_FUNCTION , SHROUD3, STANDARD_WALL_FUNCTION )
125+ WALLMODEL_KAPPA = 0.41
126+ WALLMODEL_B = 5.5
127+ WALLMODEL_MINYPLUS = 5.0
128+ WALLMODEL_MAXITER = 200
129+ WALLMODEL_RELFAC = 0.5
130+
122131% Periodic boundary marker(s) (NONE = no marker)
123132% Format: ( periodic marker, donor marker, rot_cen_x, rot_cen_y, rot_cen_z, rot_angle_x-axis, rot_angle_y-axis, rot_angle_z-axis, translation_x, translation_y, translation_z)
124133MARKER_PERIODIC = (PER1_STATOR1, PER2_STATOR1, 0.0, 0.0, 0.0, 0.0, 0.0, 8.7804878, 0.0, 0.0, 0.0, PER1_ROTOR, PER2_ROTOR, 0.0, 0.0, 0.0, 0.0, 0.0, 8.7804878, 0.0, 0.0, 0.0, PER1_STATOR2, PER2_STATOR2, 0.0, 0.0, 0.0, 0.0, 0.0, 8.7804878, 0.0, 0.0, 0.0)
@@ -167,7 +176,7 @@ TURBULENT_MIXINGPLANE= YES
167176RAMP_OUTLET_PRESSURE = NO
168177%
169178% Parameters of the outlet pressure ramp (starting outlet pressure, updating-iteration-frequency, total number of iteration for the ramp)
170- RAMP_OUTLET_PRESSURE_COEFF = (140000.0, 10 .0, 2000)
179+ RAMP_OUTLET_PRESSURE_COEFF = (140000.0, 150 .0, 2000)
171180%
172181% Specify Kind of average process for linearizing the Navier-Stokes equation at inflow and outflow BC included mixing-plane
173182% (ALGEBRAIC, AREA, MASSSFLUX, MIXEDOUT) default AREA
@@ -196,7 +205,7 @@ MARKER_MONITORING= (BLADE1, BLADE2, BLADE3)
196205NUM_METHOD_GRAD = WEIGHTED_LEAST_SQUARES
197206%
198207% Courant-Friedrichs-Lewy condition of the finest grid
199- CFL_NUMBER = 10
208+ CFL_NUMBER = 2
200209%
201210% Adaptive CFL number (NO, YES)
202211CFL_ADAPT = NO
@@ -230,8 +239,8 @@ LIMITER_ITER= 999999
230239% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
231240%
232241% Convective numerical method
233- CONV_NUM_METHOD_FLOW = ROE
234- ENTROPY_FIX_COEFF = 0.001
242+ CONV_NUM_METHOD_FLOW = JST
243+ ENTROPY_FIX_COEFF = 0.3
235244%
236245JST_SENSOR_COEFF = ( 0.5, 0.25 )
237246% Spatial numerical order integration
@@ -294,7 +303,7 @@ CONV_RESIDUAL_MINVAL= -12
294303CONV_STARTITER = 10
295304%
296305% Screen output fields (use ' SU2_CFD -d <config_file>' to view list of available fields)
297- SCREEN_OUTPUT = (OUTER_ITER, RMS_DENSITY[0], RMS_DENSITY[1], RMS_DENSITY[2], RMS_MOMENTUM-X[0], RMS_MOMENTUM-Y[0], RMS_ENERGY[0])
306+ SCREEN_OUTPUT = (OUTER_ITER, RMS_DENSITY[0], RMS_DENSITY[1], RMS_DENSITY[2], RMS_MOMENTUM-X[0], RMS_MOMENTUM-X[1], RMS_MOMENTUM-X[2], RMS_MOMENTUM- Y[0], RMS_MOMENTUM-Y[1], RMS_MOMENTUM-Y[2], RMS_MOMENTUM-Z[0], RMS_MOMENTUM-Z[1], RMS_MOMENTUM-Z[2], RMS_ENERGY[0], RMS_ENERGY[1], RMS_ENERGY[2 ])
298307%
299308% History output groups (use ' SU2_CFD -d <config_file>' to view list of available fields)
300309HISTORY_OUTPUT = (ITER, RMS_RES, TURBO_PERF)
@@ -349,7 +358,7 @@ SURFACE_FILENAME= surface_flow
349358SURFACE_ADJ_FILENAME = surface_adjoint
350359%
351360% Writing solution file frequency
352- OUTPUT_WRT_FREQ = 500
361+ OUTPUT_WRT_FREQ = 1000
353362%
354363% Writing convergence history frequency
355364HISTORY_WRT_FREQ_OUTER = 1
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