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20_Mixer_Vessel_2D_Transient: add transient turbomachinery tutorial #7

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20_Mixer_Vessel_2D_Transient: add transient turbomachinery tutorial #7

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4 changes: 4 additions & 0 deletions 20_Mixer_Vessel_2D_Transient/CASE/DATA/run.cfg
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[job_defaults]

n_threads:

189 changes: 189 additions & 0 deletions 20_Mixer_Vessel_2D_Transient/CASE/DATA/setup.xml
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<?xml version="1.0" encoding="utf-8"?><Code_Saturne_GUI case="CASE" solver_version="9.1" study="code_saturne" version="2.0">
<additional_scalars>
<users/>
</additional_scalars>
<analysis_control>
<output>
<mesh id="-1" label="Fluid domain" type="cells">
<all_variables status="on"/>
<location>all[]</location>
<writer id="-1"/>
</mesh>
<mesh id="-2" label="Boundary" type="boundary_faces">
<all_variables status="on"/>
<location>all[]</location>
<writer id="-1"/>
</mesh>
<probe_format choice="CSV"/>
<probe_recording_frequency>1</probe_recording_frequency>
<probes_interpolation choice=""/>
<probes_snap choice=""/>
<writer id="-1" label="results">
<directory name="postprocessing"/>
<format name="ensight" options="separate_meshes"/>
<frequency period="time_step">100</frequency>
<output_at_end status="on"/>
<time_dependency choice="transient_connectivity"/>
</writer>
</output>
<profiles/>
<time_averages/>
<time_parameters>
<maximum_time>5</maximum_time>
<max_courant_num>0.5</max_courant_num>
<property name="courant_number" label="CourantNb"/>
<property name="fourier_number" label="FourierNb"/>
<time_passing>0</time_passing>
<time_step_ref>0.001</time_step_ref>
</time_parameters>
</analysis_control>
<boundary_conditions>
<boundary label="rotor_wall" name="1" nature="wall">rotor</boundary>
<boundary label="stator_wall" name="2" nature="wall">stator</boundary>
<boundary label="front" name="3" nature="symmetry">front</boundary>
<boundary label="back" name="4" nature="symmetry">back</boundary>
<wall label="rotor_wall" field_id="none">
<velocity_pressure choice="off"/>
</wall>
<wall label="stator_wall" field_id="none">
<velocity_pressure choice="off"/>
</wall>
<symmetry label="front" field_id="none"/>
<symmetry label="back" field_id="none"/>
</boundary_conditions>
<calculation_management>
<start_restart>
<frozen_field status="off"/>
</start_restart>
</calculation_management>
<lagrangian model="off"/>
<numerical_parameters>
<velocity_pressure_algo choice="simplec"/>
</numerical_parameters>
<physical_properties>
<fluid_properties>
<material choice="user_material"/>
<method choice="user_properties"/>
<property name="density" choice="constant" label="Density">
<initial_value>1</initial_value>
<listing_printing status="off"/>
<postprocessing_recording status="off"/>
</property>
<property name="molecular_viscosity" choice="constant" label="LamVisc">
<initial_value>1e-05</initial_value>
<listing_printing status="off"/>
<postprocessing_recording status="off"/>
</property>
<reference_pressure>101325</reference_pressure>
<reference_temperature>293.15</reference_temperature>
</fluid_properties>
<gravity>
<gravity_x>0</gravity_x>
<gravity_y>0</gravity_y>
<gravity_z>0</gravity_z>
</gravity>
<notebook/>
<omega>
<omega_x>0</omega_x>
<omega_y>0</omega_y>
<omega_z>0</omega_z>
</omega>
<time_tables/>
</physical_properties>
<solution_domain>
<extrusion/>
<faces_cutting status="off"/>
<joining/>
<mesh_smoothing status="off"/>
<meshes_list>
<mesh name="rotor.msh"/>
<mesh name="stator.msh"/>
</meshes_list>
<periodicity/>
<thin_walls/>
<volumic_conditions>
<zone label="all_cells" id="1" initialization="on" physical_properties="on">all[]</zone>
<zone label="rotor_fluid" id="2">rotor_fluid</zone>
<zone label="stator_fluid" id="3">stator_fluid</zone>
</volumic_conditions>
</solution_domain>
<thermophysical_models>
<ale_method/>
<atmospheric_flows model="off">
<large_scale_meteo status="off"/>
<read_meteo_data status="off"/>
</atmospheric_flows>
<compressible_model model="off"/>
<conjugate_heat_transfer>
<external_coupling>
<syrthes_instances/>
</external_coupling>
</conjugate_heat_transfer>
<gas_combustion model="off">
<thermodynamical_pressure status="off"/>
</gas_combustion>
<immersed_boundaries/>
<internal_coupling>
<coupled_scalars/>
<solid_zones/>
</internal_coupling>
<porosities/>
<radiative_transfer model="off"/>
<reference_values>
<length/>
</reference_values>
<source_terms/>
<thermal_scalar model="off"/>
<turbomachinery model="transient">
<joining>
<face_joining name="1">
<selector>AMI1 or AMI2</selector>
<fraction>0.1</fraction>
<plane>25</plane>
<verbosity>0</verbosity>
<visualization>0</visualization>
</face_joining>
</joining>
<rotor rotor_id="0">
<criteria>rotor_fluid</criteria>
<rotation>
<axis_x>0</axis_x>
<axis_y>0</axis_y>
<axis_z>1</axis_z>
<invariant_x>0</invariant_x>
<invariant_y>0</invariant_y>
<invariant_z>0</invariant_z>
</rotation>
<velocity status="constant">
<value>6.2832</value>
</velocity>
</rotor>
</turbomachinery>
<turbulence model="off">
<initialization zone_id="1" choice="reference_value"/>
<reference_velocity>1</reference_velocity>
<wall_function>0</wall_function>
</turbulence>
<velocity_pressure>
<initialization>
<formula zone_id="1">velocity[0] = 0.;
velocity[1] = 0.;
velocity[2] = 0.;</formula>
</initialization>
<property name="stress" label="Stress" support="boundary"/>
<property name="stress_normal" label="Stress, normal" support="boundary">
<postprocessing_recording status="off"/>
</property>
<property name="stress_tangential" label="Stress, tangential" support="boundary">
<postprocessing_recording status="off"/>
</property>
<property name="total_pressure" label="total_pressure"/>
<property name="yplus" label="Yplus" support="boundary"/>
<variable name="pressure" label="Pressure"/>
<variable name="velocity" dimension="3" label="Velocity"/>
</velocity_pressure>
</thermophysical_models>
<user_functions>
<calculator/>
</user_functions>
</Code_Saturne_GUI>
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