Skip to content

19_Mixer_Vessel_2D: add frozen rotor turbomachinery tutorial #6

New issue

Have a question about this project? Sign up for a free GitHub account to open an issue and contact its maintainers and the community.

Sign up for GitHub

By clicking “Sign up for GitHub”, you agree to our terms of service and privacy statement. We’ll occasionally send you account related emails.

Already on GitHub? Sign in to your account

Open
florian-simvia wants to merge 1 commit into
base: main
Choose a base branch
from
Open

19_Mixer_Vessel_2D: add frozen rotor turbomachinery tutorial #6

Show file tree
Hide file tree
Changes from all commits
Commits
Show all changes
1 commit
Select commit
File filter

Filter by extension

Filter by extension
Conversations
Failed to load comments.
Loading
Jump to
Jump to file
Failed to load files.
Loading
Diff view
Diff view
5 changes: 5 additions & 0 deletions 19_Mixer_Vessel_2D/CASE/DATA/run.cfg
View file
Open in desktop
Original file line number Diff line number Diff line change
@@ -0,0 +1,5 @@
[job_defaults]

n_threads: 1
n_procs: 1

207 changes: 207 additions & 0 deletions 19_Mixer_Vessel_2D/CASE/DATA/setup.xml
View file
Open in desktop
Original file line number Diff line number Diff line change
@@ -0,0 +1,207 @@
<?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">1</frequency>
<output_at_end status="on"/>
<time_dependency choice="fixed_mesh"/>
</writer>
</output>
<profiles/>
<time_averages/>
<time_parameters>
<iterations>100</iterations>
<property name="courant_number" label="CourantNb"/>
<property name="fourier_number" label="FourierNb"/>
<time_passing>0</time_passing>
<time_step_ref>0.01</time_step_ref>
</time_parameters>
</analysis_control>
<boundary_conditions>
<boundary label="walls" name="1" nature="wall">walls</boundary>
<boundary label="z0" name="2" nature="symmetry">z0</boundary>
<boundary label="z1" name="3" nature="symmetry">z1</boundary>
<wall label="walls" field_id="none">
<velocity_pressure choice="off"/>
</wall>
<symmetry label="z0" field_id="none"/>
<symmetry label="z1" 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>
</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="mixerVessel2D.msh"/>
</meshes_list>
<periodicity/>
<thin_walls>
<thin_wall name="1">
<selector>plane[0, 1, 0, 0, 0.001] and cylinder[0, 0, -1, 0, 0, 1, 0.05]</selector>
</thin_wall>
<thin_wall name="2">
<selector>plane[1, 0, 0, 0, 0.001] and cylinder[0, 0, -1, 0, 0, 1, 0.05]</selector>
</thin_wall>
<thin_wall name="3">
<selector>plane[0.7071, 0.7071, 0, 0, 0.001] and cylinder[0, 0, -1, 0, 0, 1, 0.1] and not cylinder[0, 0, -1, 0, 0, 1, 0.07]</selector>
</thin_wall>
<thin_wall name="4">
<selector>plane[-0.7071, 0.7071, 0, 0, 0.001] and cylinder[0, 0, -1, 0, 0, 1, 0.1] and not cylinder[0, 0, -1, 0, 0, 1, 0.07]</selector>
</thin_wall>
<thin_wall name="5">
<selector>plane[0.7071, -0.7071, 0, 0, 0.001] and cylinder[0, 0, -1, 0, 0, 1, 0.1] and not cylinder[0, 0, -1, 0, 0, 1, 0.07]</selector>
</thin_wall>
<thin_wall name="6">
<selector>plane[-0.7071, -0.7071, 0, 0, 0.001] and cylinder[0, 0, -1, 0, 0, 1, 0.1] and not cylinder[0, 0, -1, 0, 0, 1, 0.07]</selector>
</thin_wall>
</thin_walls>
<volumic_conditions>
<zone label="all_cells" id="1" initialization="on" physical_properties="on">all[]</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="frozen">
<joining/>
<rotor rotor_id="0">
<criteria>cylinder[0, 0, -0.1, 0, 0, 0.1, 0.06]</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>104.72</value>
</velocity>
</rotor>
</turbomachinery>
<turbulence model="k-epsilon-PL">
<initialization zone_id="1" choice="reference_value"/>
<reference_velocity>5</reference_velocity>
<variable name="k" label="TurbEner">
<rhs_reconstruction>1</rhs_reconstruction>
<solver_precision>1e-05</solver_precision>
<relaxation>0.5</relaxation>
</variable>
<variable name="epsilon" label="Dissipation">
<rhs_reconstruction>1</rhs_reconstruction>
<solver_precision>1e-05</solver_precision>
<relaxation>0.5</relaxation>
</variable>
<wall_function>3</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">
<rhs_reconstruction>2</rhs_reconstruction>
<relaxation>0.3</relaxation>
</variable>
<variable name="velocity" dimension="3" label="Velocity">
<rhs_reconstruction>1</rhs_reconstruction>
<relaxation>0.5</relaxation>
</variable>
</velocity_pressure>
</thermophysical_models>
<user_functions>
<calculator/>
</user_functions>
</Code_Saturne_GUI>
Loading