A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.
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Updated
Feb 28, 2025 - Fortran
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.
analytical solver for laval nozzle flow with sonic shock
A modern, unstructured, subsonic/supersonic flow solver.
A compact Finite Volume Method solver for 2D Euler equations (internal channel flow). Demonstrates numerical methods, scientific programming and shock capturing.
Python tool for generating supersonic impulse turbine blade geometry with MOC, vortex‑flow theory, and CAD‑ready contours.
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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