A panel-based flow solver. Currently in beta but with working solvers for incompressible and inviscid hypersonic flow.
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Updated
Feb 28, 2022 - Python
A panel-based flow solver. Currently in beta but with working solvers for incompressible and inviscid hypersonic flow.
Discrete vortex panel method
Calculate common 2D airfoil parameters by just setting a few inputs and drawing the geometry of the body in a dynamic way
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