There are 0 repository under xfoil topic.
Aircraft design optimization made fast through computational graph transformations (e.g., automatic differentiation). Composable analysis tools for aerodynamics, propulsion, structures, trajectory design, and much more.
NeuralFoil is a practical airfoil aerodynamics analysis tool using physics-informed machine learning, exposed to end-users in pure Python/NumPy.
An all in one airfoil modelling, meshing, analysis, and optimization tool with built in support for gmsh, SU2, and xfoil
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
PythonXfoil is a Python module that provides an interface to natively and intuitively run concurrent aerodynamic analyses using XFOIL. It allows users to define airfoil geometries, set analysis parameters, and execute XFOIL simulations programmatically. Its focus is to provide an intuitive and easy-to-use alternative to similar modules.
Source code of my master's thesis: "Development of an automated design and optimization program for anisotropic UAV propellers"
An aerodynamic shape optimization algorithm for 2D airfoils.
Computes aerodynamical coefficients related to the flow around an airfoil.
Efficient Foil Shape Optimization Using Artificial Neural Network-Based Surrogate Model with Adaptive Sampling Strategy
Uses Xfoil to obtain polar data and plot polar graphs of user entered naca airfoils on a pdf. Easy way to get custom Xfoil data and plots
Low-Windspeed Airfoil Optimization for Bikes
The lists of the projects that I have completed during my university.
Visualisation of general XFOIL results
Panel method for steady multi-component 2D airfoil analysis using a linear vortex distribution | Python version
Fork of the original repository by Rafael Oliveira. Launch XFOIL from MATLAB