├── .flake8 ├── .git-blame-ignore-revs ├── .github └── workflows │ ├── black.yml │ ├── flake8.yml │ ├── host_docs.yml │ ├── isort.yml │ ├── release_workflow.yml │ └── unit_tests_and_docs.yml ├── .gitignore ├── .vscode ├── extensions.json └── settings.json ├── LICENSE ├── README.md ├── docs ├── Makefile ├── _exts │ ├── __init__.py │ ├── embed_bibtex.py │ ├── embed_code.py │ ├── embed_compare.py │ ├── embed_n2.py │ ├── embed_options.py │ ├── embed_pregen_n2.py │ ├── embed_shell_cmd.py │ ├── link_class_from_docstring.py │ └── tags.py ├── _n2html │ └── .gitkeep ├── _theme │ ├── static │ │ ├── searchtools.js │ │ └── style.css │ └── theme.conf ├── basics │ ├── builders.rst │ ├── model_assembly.rst │ ├── model_hierarchy.rst │ ├── mphys_model_assembly.png │ ├── multipoint_example.png │ ├── naming_conventions.rst │ ├── remote_components.rst │ ├── scenario_example.png │ └── tagged_promotion.rst ├── conf.py ├── developers │ ├── mphys_group.rst │ └── new_multiphysics_problems.rst ├── index.rst ├── logo │ ├── mphys_logo_no_background.png │ └── mphys_logo_white_behind_mesh.png ├── make.bat ├── references │ ├── citing_mphys.rst │ ├── papers_using_mphys.bib │ └── papers_using_mphys.rst └── scenarios │ ├── aerodynamic.rst │ ├── aerostructural.rst │ └── structural.rst ├── examples ├── aero_only │ └── mach_tutorial_wing │ │ ├── adflow │ │ ├── mphys_aero_analysis.py │ │ ├── mphys_aero_opt.py │ │ ├── mphys_aero_opt_2pt.py │ │ ├── mphys_aero_opt_2pt_parallel.py │ │ └── readme.md │ │ └── vlm │ │ ├── README.md │ │ ├── run_vlm.py │ │ ├── run_vlm_2scenarios.py │ │ └── run_vlm_2scenarios_parallel.py ├── aerostructural │ ├── crm_with_tail │ │ └── vlm_meld_pyshell │ │ │ ├── CRM_VLM_mesh_extended_coarse.dat │ │ │ ├── CRM_VLM_mesh_extended_coarse_tail.dat │ │ │ ├── CRM_VLM_tail.dat │ │ │ ├── CRM_box_2nd.bdf │ │ │ ├── CRM_box_2nd_tailbox.bdf │ │ │ ├── main_as_mphys.py │ │ │ ├── mappings.py │ │ │ └── util_components.py │ ├── mach_tutorial_wing │ │ ├── adflow_meld_tacs │ │ │ ├── mphys_as_2scenario.py │ │ │ ├── readme.md │ │ │ └── tacs_setup.py │ │ └── vlm_meld_tacs │ │ │ ├── README.md │ │ │ ├── as_opt.py │ │ │ ├── component_list.txt │ │ │ ├── run_analysis.py │ │ │ ├── run_analysis_parallel.py │ │ │ ├── struct_dv_components.py │ │ │ ├── tacs_setup.py │ │ │ ├── wing_VLM.dat │ │ │ └── wingbox_Y_Z_flip.bdf │ ├── oas_tacs_wing │ │ ├── README.md │ │ ├── run_oas_tacs_wing.py │ │ ├── tacs_setup.py │ │ ├── twin_aisle_aircraft.vsp3 │ │ └── wingbox.bdf │ └── supersonic_panel │ │ ├── README │ │ ├── aerodynamics_mphys.py │ │ ├── as_opt_parallel.py │ │ ├── as_opt_remote_parallel.py │ │ ├── as_opt_remote_serial.py │ │ ├── beam_solver.py │ │ ├── geometry_morph.py │ │ ├── mphys_server.py │ │ ├── piston_theory.py │ │ ├── run.py │ │ ├── run_parallel.py │ │ ├── structures_mphys.py │ │ ├── xfer.py │ │ └── xfer_mphys.py ├── aerothermal │ └── conjugate_hx_naca0012 │ │ ├── ffds │ │ └── n0012_ffd.xyz │ │ └── run_opt.py ├── struct_only │ ├── beam_shape_opt │ │ ├── Slender_Beam.bdf │ │ ├── ffd_8_linear.fmt │ │ └── shape_opt.py │ ├── crm9 │ │ ├── README.md │ │ ├── pyopt_mass_min.py │ │ ├── run_tacs_mphys.py │ │ ├── tacs_analysis.py │ │ └── tacs_setup.py │ ├── mach_tutorial_wing │ │ └── mphys_struct.py │ └── tank_shape_opt │ │ ├── run_tacs_mphys.py │ │ ├── tank.dat │ │ └── tank.vsp3 └── time_domain │ ├── README.md │ ├── builder_version │ ├── aero_solver.py │ ├── run.py │ ├── struct_solver.py │ └── xfer_scheme.py │ ├── modal_comps.py │ ├── prototype │ ├── modal_comps.py │ ├── timestep_groups │ │ ├── modal_comps.py │ │ ├── modal_integrate.py │ │ ├── sphere_body1_mode1.dat │ │ └── sphere_body1_mode2.dat │ └── timestep_loop │ │ ├── modal_comps.py │ │ ├── modal_integrate.py │ │ ├── modal_integrator.py │ │ ├── sphere_body1_mode1.dat │ │ └── sphere_body1_mode2.dat │ ├── sphere_body1_mode1.dat │ └── sphere_body1_mode2.dat ├── mphys ├── __init__.py ├── core │ ├── __init__.py │ ├── builder.py │ ├── coupling_group.py │ ├── distributed_converter.py │ ├── distributed_summer.py │ ├── mask_converter.py │ ├── mphys_group.py │ ├── multipoint.py │ ├── scenario.py │ └── variable_convention.py ├── integrated_forces.py ├── network │ ├── __init__.py │ ├── remote_component.py │ ├── server.py │ ├── server_manager.py │ └── zmq_pbs.py ├── scenarios │ ├── __init__.py │ ├── aerodynamic.py │ ├── aeropropulsive.py │ ├── aerostructural.py │ ├── aerothermal.py │ ├── geo_disp.py │ └── structural.py ├── time_domain │ ├── integator_aerostructural.py │ ├── integrator.py │ ├── time_domain_builder.py │ ├── time_domain_variables.py │ ├── timestep.py │ └── timestep_aerostructural.py └── utils │ ├── __init__.py │ ├── directory_utils.py │ └── docs │ ├── _utils │ ├── __init__.py │ ├── docutil.py │ ├── generate_sourcedocs.py │ ├── patch.py │ ├── preprocess_tags.py │ ├── run_sub.py │ └── upload_doc_version.py │ └── config_params.py ├── pyproject.toml ├── setup.py └── tests ├── input_files └── get-input-files.sh ├── integration_tests ├── test_adflow_derivs.py ├── test_con_derivs.py ├── test_dafoam_derivs.py ├── 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