Community Computational Fluid Dynamics Turbo Python API in the Simulation context

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Python API in the Simulation context

cfd enthusiast

Hello Everyone,

I am currently writing a script to automate the simulation context.

In the simulation context I want to access the static pressure of the inlet and outlet in the Turbo initial solution tab.

I belive I have to fill them out correctly if i choose "for turbomachinery" in the initial solution tab under one of the domains.

I can't find the code to set those static pressures in the API user manual.

 

  • +1

    Hi,

    The static pressures can be accessed through the commands:

     set_inlet_initial_static_pressure(v)

    set_outlet_initial_static_pressure(v)

    So for the tutorial of the multistage axial compressor it writes for example in this way:

    ## InititalConditions
    # Domain1 Settings
    main_flow_par = dom_parameters.InitialSolutionParameters.MainFlowVariablesParameters(domain1)
    main_flow_par.set_initial_solution_choice('Turbo')
    domain1.set_inlet_initial_static_pressure(90000)

    tur_flow_par = dom_parameters.InitialSolutionParameters.TurbulentQuantitiesParameters.InitialValuesParameters(domain1)
    tur_flow_par.set_k_free(150)
    tur_flow_par.set_epsilon_free(12587e4)

    #Domain2 Settings
    print("Row 2: Rotating?",domain2.is_rotating())
    main_flow_par2 = dom_parameters.InitialSolutionParameters.MainFlowVariablesParameters(domain2)
    main_flow_par2.set_initial_solution_choice('Turbo')
    domain2.set_inlet_initial_static_pressure(85000)
    domain2.set_outlet_initial_static_pressure(100000)

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