Buffalo Wings Documentation

Buffalo Wings is a Python geometry library for building airfoil and wing models from aerodynamic definitions. It is designed to support interactive design workflows, visualization tools, and downstream analysis or meshing pipelines.

Note

This project is under development and the API might change between releases.

Start Here

If you are new to the project, start with the examples page for working airfoil and wing scripts built on the public API. The airfoil subsystem is currently the most mature part of the project, while the wing subsystem is still evolving.

• New users should begin with Examples.

• API-oriented users should go to Library Interface.

• Contributors should start with Developer Resources.

Project Focus

The public API is centered on buffalo_wings.airfoil, buffalo_wings.wing, and buffalo_wings.type_aliases. The project is being developed as both a usable Python library and a geometry foundation for future GUI-based airfoil and wing design tools. Buffalo Wings is not intended to be a general-purpose CAD system.

Contents

• Home
• Examples
• Specifications
• Command Line Interface
• Library Interface
• Developer Resources
• License
• Changes
• Project