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MachLine (Multi-order Approach to Calculating High-speed Linear 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. MachLine 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.
MachLine is under active development and is not yet fully capable. We anticipate development to be completed sometime in the summer of 2023.