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This repository has been archived by the owner on Jan 11, 2022. It is now read-only.
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.