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Welcome to the TriPan wiki!

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TriPan (Triangular Panel Aerodynamics) is a modern, unstructured, subsonic/supersonic flow solver currently being developed by the AeroLab. It is a linear panel method based on the Prandtl-Glauert equation. TriPan will implement many features not available in legacy compressible panel methods, such as unstructured meshes, iterative matrix solvers, automatic wake modelling, low-order singularity distributions, and more.

TriPan is under active development and is not yet fully capable. We anticipate development to be completed sometime in the summer of 2023.

Literature

Installation

[Running TriPan](Running TriPan)

[Input File Structure](Input File Structure)

[Common Issues](Common Issues)

Support