A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.

Physics-informed neural networks for highly compressible flows 🧠🌊

A framework to implement CHEMically reacting Method Of Characteristics for supersonic reacting flows.

A MATLAB code incorporating the analysis method described by Barrowman (1967) to analyse the aerodynamic properties of a supersonic sounding rocket.

analytical solver for laval nozzle flow with sonic shock

A modern, unstructured, subsonic/supersonic flow solver.