Ptera Software is a fast, easy-to-use, and open-source software package for analyzing flapping-wing flight.
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.
Calculate common 2D airfoil parameters by just setting a few inputs and drawing the geometry of the body in a dynamic way
Discrete vortex panel method
XFOIL 6.99 airfoil analysis code -- ready to build on macOS Apple Silicon (M1/M2/M3/M4/M5/etc.) with gfortran and XQuartz. Subsonic airfoil design, panel method, boundary layer analysis.
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.
A modern, unstructured, subsonic/supersonic flow solver.
High Performance CPU/GPU Potential Flow Solver
Computational aerodynamics laboratory project implementing Hess-Smith panel method and Weissinger lifting-line theory for airfoil and wing analysis
Efficient Foil Shape Optimization Using Artificial Neural Network-Based Surrogate Model with Adaptive Sampling Strategy
Panel-based boundary integral equation solver for 2D Laplace problems using Nystrom discretization.
Hyunbin Kang's Portfolio
Build and run XFOIL 6.99 for airfoil analysis on macOS Apple Silicon with patched source and GUI support via XQuartz.
Analyze aerodynamic properties using panel methods and lifting-line theory, facilitating effective airfoil and wing design for aerospace applications.
Panel method solver and UI application with Streamlit
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