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metadata.json
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46 lines (46 loc) · 1.8 KB
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{
"parser": "github",
"uid": "github/coding4Acause/PANKH",
"url": "https://github.com/coding4Acause/PANKH",
"data": {
"doi": "https://doi.org/10.5281/zenodo.17413805",
"name": "PANKH",
"url": "https://github.com/coding4Acause/PANKH",
"full_name": "coding4Acause/PANKH",
"html_url": "https://github.com/coding4Acause/PANKH",
"description": "PANKH (Panel Analysis of uNsteady Kinematics of Hovering airfoils) is a solver for studying unsteady aerodynamics of flapping and hovering airfoils using the unsteady vortex panel method. This repository includes the source code, example cases, and validation results. ",
"created_at": "2025-03-15T18:01:22Z",
"updated_at": "2025-11-10T17:23:19Z",
"clone_url": "https://github.com/coding4Acause/PANKH.git",
"size": 26471,
"stargazers_count": 2,
"watchers_count": 2,
"language": "C++",
"open_issues_count": 2,
"license": {
"key": "mit",
"name": "MIT License",
"spdx_id": "MIT",
"url": "https://api.github.com/licenses/mit",
"node_id": "MDc6TGljZW5zZTEz"
},
"subscribers_count": 3,
"owner": {
"html_url": "https://github.com/coding4Acause",
"avatar_url": "https://avatars.githubusercontent.com/u/199661758?v=4",
"login": "coding4Acause",
"type": "User"
},
"topics": [
"airfoils",
"kutta-schukowski",
"naca",
"potential-flow-theory",
"unsteady-flows",
"vortex-panel-method",
"kutta-condition"
],
"timestamp": "2025-11-16 00:56:20.546340",
"avatar": "https://avatars.githubusercontent.com/u/199661758?v=4"
}
}