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Aircraft design optimization made fast through modern automatic differentiation. Composable analysis tools for aerodynamics, propulsion, structures, trajectory design, and much more.
NeuralFoil is an airfoil aerodynamics analysis tool using physics-informed machine learning, in pure Python/NumPy.
This repository contains code development for the 4th credit project for AE416. The aim of the project is to compare different optimization algorithms in the context of airfoil optimization.
Julia wrapper for the 2D airfoil panel code XFOIL
Python scripts related to aerodynamic analysis and shape optimization
Stripped down version of XFOIL as compiled python module.
Tools for airfoil polar preparation and processing
Analyse any airfoil from UIUC database in xfoil and obtain results.
ANN based Surrogate model optimization of airfoil using XFOIL
Source code of my master's thesis: "Development of an automated design and optimization program for anisotropic UAV propellers"
Low-Windspeed Airfoil Optimization for Bikes
The lists of the projects that I have completed during my university.
Visualisation of general XFOIL results
Fork of the original repository by Rafael Oliveira. Launch XFOIL from MATLAB