{"id":24259115,"url":"https://github.com/paulcreusy/flight-mech","last_synced_at":"2025-03-04T21:24:16.515Z","repository":{"id":272330780,"uuid":"916071439","full_name":"PaulCreusy/flight-mech","owner":"PaulCreusy","description":"Python package to compute the characteristics of an airplane or an airfoil based on simple flight mechanics equations.","archived":false,"fork":false,"pushed_at":"2025-03-03T21:38:40.000Z","size":9295,"stargazers_count":2,"open_issues_count":16,"forks_count":0,"subscribers_count":1,"default_branch":"main","last_synced_at":"2025-03-03T22:28:29.400Z","etag":null,"topics":["airfoil","airfoil-analysis","airplane","flight-mech","flight-mechanics","python","turbojet","wings"],"latest_commit_sha":null,"homepage":"https://flight-mech.creusy.fr","language":"Python","has_issues":true,"has_wiki":null,"has_pages":null,"mirror_url":null,"source_name":null,"license":"mit","status":null,"scm":"git","pull_requests_enabled":true,"icon_url":"https://github.com/PaulCreusy.png","metadata":{"files":{"readme":"README.md","changelog":null,"contributing":null,"funding":null,"license":"LICENSE","code_of_conduct":null,"threat_model":null,"audit":null,"citation":null,"codeowners":null,"security":null,"support":null,"governance":null,"roadmap":null,"authors":null,"dei":null,"publiccode":null,"codemeta":null}},"created_at":"2025-01-13T12:01:09.000Z","updated_at":"2025-03-02T16:56:08.000Z","dependencies_parsed_at":"2025-01-13T18:49:23.180Z","dependency_job_id":"33f34f01-a62b-4a8f-9d07-364cad945879","html_url":"https://github.com/PaulCreusy/flight-mech","commit_stats":null,"previous_names":["paulcreusy/flight-mechanics-calculator","paulcreusy/flight-mech"],"tags_count":5,"template":false,"template_full_name":null,"repository_url":"https://repos.ecosyste.ms/api/v1/hosts/GitHub/repositories/PaulCreusy%2Fflight-mech","tags_url":"https://repos.ecosyste.ms/api/v1/hosts/GitHub/repositories/PaulCreusy%2Fflight-mech/tags","releases_url":"https://repos.ecosyste.ms/api/v1/hosts/GitHub/repositories/PaulCreusy%2Fflight-mech/releases","manifests_url":"https://repos.ecosyste.ms/api/v1/hosts/GitHub/repositories/PaulCreusy%2Fflight-mech/manifests","owner_url":"https://repos.ecosyste.ms/api/v1/hosts/GitHub/owners/PaulCreusy","download_url":"https://codeload.github.com/PaulCreusy/flight-mech/tar.gz/refs/heads/main","host":{"name":"GitHub","url":"https://github.com","kind":"github","repositories_count":241753016,"owners_count":20014247,"icon_url":"https://github.com/github.png","version":null,"created_at":"2022-05-30T11:31:42.601Z","updated_at":"2022-07-04T15:15:14.044Z","host_url":"https://repos.ecosyste.ms/api/v1/hosts/GitHub","repositories_url":"https://repos.ecosyste.ms/api/v1/hosts/GitHub/repositories","repository_names_url":"https://repos.ecosyste.ms/api/v1/hosts/GitHub/repository_names","owners_url":"https://repos.ecosyste.ms/api/v1/hosts/GitHub/owners"}},"keywords":["airfoil","airfoil-analysis","airplane","flight-mech","flight-mechanics","python","turbojet","wings"],"created_at":"2025-01-15T05:54:17.965Z","updated_at":"2025-03-04T21:24:16.503Z","avatar_url":"https://github.com/PaulCreusy.png","language":"Python","funding_links":[],"categories":[],"sub_categories":[],"readme":"# Flight-mech\n\n![PyPI - Version](https://img.shields.io/pypi/v/flight-mech)![PyPI - Downloads](https://img.shields.io/pypi/dm/flight-mech)![Pylint Badge](https://github.com/PaulCreusy/flight-mech/actions/workflows/pylint.yml/badge.svg)![Pytest Badge](https://github.com/PaulCreusy/flight-mech/actions/workflows/pytest.yml/badge.svg)\n\n## License\n\nThis software has been developed by Paul Creusy and is shared under the MIT License.\n\n## Getting started\n\n### Installation\n\n#### Pip installation\n\nTo install this module with pip, please use:\n\n```bash\npip install flight-mech\n```\n\n#### Manual installation\n\nFor a manual installation, please clone the repository and install the required Python libraries using the command:\n\n```bash\npip install -r requirements.txt\n```\n\n### Documentation\n\nThe documentation is available online [here](https://flight-mech.creusy.fr).\n\nOtherwise, if you decided to clone the repository, you can generate the documentation using the following commands:\n\n```bash\ncd docs\nmake html\n```\n\nAnd open the file `docs/_build/html/index.html` in your browser. \n\n### Functionalities\n\nThis software includes various modules to build a numerical plane model and compute its characteristics. The modules implemented are the following:\n\n- `atmosphere` : defines several atmosphere models to compute density, temperature, pressure and other quantities.\n- `aerodynamics` : contains functions to compute quantities in the boundary layer of a fluid flow.\n- `airfoil` : allows to define the geometry of an airfoil and compute the lift and moment coefficients.\n- `wing` : allows to define the geometry of a wing and compute the lift and drag coefficients.\n- `fuel` : defines several types of broadly used fuels in aeronautics.\n- `turbine` : allows to define several types of turbine to compute their thrust and consumption at various operating conditions.\n- `plane` : allows to define a numerical plane model, binding the previous modules, to compute its flight characteristics. \n","project_url":"https://awesome.ecosyste.ms/api/v1/projects/github.com%2Fpaulcreusy%2Fflight-mech","html_url":"https://awesome.ecosyste.ms/projects/github.com%2Fpaulcreusy%2Fflight-mech","lists_url":"https://awesome.ecosyste.ms/api/v1/projects/github.com%2Fpaulcreusy%2Fflight-mech/lists"}