A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.
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Updated
Nov 23, 2024 - Fortran
A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.
A panel-based flow solver. Currently in beta but with working solvers for incompressible and inviscid hypersonic flow.
Discrete vortex panel method
This project is prepared as part of CA course and it contains a study on the 2 dimensional Hess-Smith panel method (HSPM) for a cambered airfoil, NACA 1408.
Calculate common 2D airfoil parameters by just setting a few inputs and drawing the geometry of the body in a dynamic way
High Performance CPU/GPU Potential Flow Solver
A modern, unstructured, subsonic/supersonic flow solver.
Hyunbin Kang's Portfolio
Efficient Foil Shape Optimization Using Artificial Neural Network-Based Surrogate Model with Adaptive Sampling Strategy
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