usuaero / PyPan

A panel-based flow solver. Currently in beta but with working solvers for incompressible and inviscid hypersonic flow.

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PyPan

The greatest thing since PAN AIR.

Vortex rollup on a swept wing as predicted by PyPan.

Documentation

Check out the documentation at ReadTheDocs.

About

A panel-based flow solver. Currently in beta but with working solvers for incompressible and inviscid hypersonic flow.

License:MIT License


Languages

Language:Python 100.0%