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.
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Updated
Mar 18, 2017 - Python
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.
Python scripts related to aerodynamic analysis and shape optimization
Analyse any airfoil from UIUC database in xfoil and obtain results.
Stripped down version of XFOIL as compiled python module.
Low-Windspeed Airfoil Optimization for Bikes
Julia wrapper for the 2D airfoil panel code XFOIL
A CNN Model for Estimating Airfoil Aerodynamic Lift and Drag Coefficients.
Source code of my master's thesis: "Development of an automated design and optimization program for anisotropic UAV propellers"
翼型をNSGA3によって最適化するプログラム。新翼型のモデル手法として、既存翼型の混合とスプライン曲線の2種がある
An all in one airfoil modelling, meshing, analysis, and optimization tool with built in support for gmsh, SU2, and xfoil
Fork of the original repository by Rafael Oliveira. Launch XFOIL from MATLAB
Visualisation of general XFOIL results
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