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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 MATLAB code incorporating the analysis method described by Barrowman (1967) to analyse the aerodynamic properties of a supersonic sounding rocket.
A modern, unstructured, subsonic/supersonic flow solver.
analytical solver for laval nozzle flow with sonic shock
A compact Finite Volume Method solver for 2D Euler equations (internal channel flow). Demonstrates numerical methods, scientific programming and shock capturing.
To model supersonic flow around a bullet, calculate Cd and drag forces using MATLAB, and validate these with Fluent CFD simulations, comparing analytical and numerical approaches for accuracy.
A framework to implement CHEMically reacting Method Of Characteristics for supersonic reacting flows.
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