chiefenne / PyAeroLinks
PyAero is an open-source airfoil contour analysis and CFD meshing tool.
☆227Updated 4 months ago
Alternatives and similar repositories for PyAero
Users that are interested in PyAero are comparing it to the libraries listed below
Sorting:
- OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.☆243Updated 3 months ago
- DAFoam: Discrete Adjoint with OpenFOAM for High-fidelity Multidisciplinary Design Optimization☆304Updated last week
- MACH: MDO of Aircraft Configurations with High fidelity☆148Updated 2 months ago
- Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code☆171Updated 2 weeks ago
- Multiphysics with OpenMDAO☆115Updated last month
- ADflow is a finite volume RANS solver tailored for gradient-based aerodynamic design optimization.☆290Updated last month
- CEASIOMpy is a Python conceptual aircraft design environment☆134Updated this week
- Python interface for XFOIL. The objective of this library is to be able to be able to call XFOIL from Python iteratively for any simulati…☆76Updated 4 years ago
- NeuralFoil is a practical airfoil aerodynamics analysis tool using physics-informed machine learning, exposed to end-users in pure Python…☆349Updated 2 months ago
- An interactional aerodynamics and acoustics solver for multirotor aircraft and wind energy☆347Updated 4 months ago
- CFD for Everyone☆146Updated 5 months ago
- Hypersonic / Rarefied gas dynamics code developments (GPL-3.0)☆253Updated 2 years ago
- The market leading open-source GUI for OpenFOAM®☆137Updated 10 months ago
- pyGeo provides geometric design variables and constraints suitable for gradient-based optimization.☆196Updated last month
- Stripped down version of XFOIL as compiled python module☆108Updated 4 years ago
- Thermodynamic cycle modeling library, built on top of OpenMDAO☆149Updated 3 months ago
- Finite-element library for analysis and adjoint-based gradient evaluation☆138Updated 2 weeks ago
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python☆80Updated 3 years ago
- An all in one airfoil modelling, meshing, analysis, and optimization tool with built in support for gmsh, SU2, and xfoil☆41Updated 7 months ago
- A CFD solver for multi-component compressible flow with application to high-explosive detonation, explosive safety and air blast☆284Updated 2 weeks ago
- The Python XFOIL optimization toolbox can be used to optimize airfoils for a specific operating range, and might be useful to you for its…☆49Updated 8 years ago
- ☆327Updated 3 years ago
- Tucan remains among the simplest and most user friendly programs for aerodynamics based on vortex lattice methods. This project is unique…☆79Updated last year
- Source and vortex panel method codes referenced in my YouTube videos.☆109Updated 5 years ago
- CFDTool - An easy to use OpenFOAM / SU2 / CFD simulation toolbox☆107Updated 5 months ago
- SnappyHexMesh GUI Addon for Blender☆116Updated last week
- Python classes for easier creation of OpenFOAM's blockMesh dictionaries.☆192Updated last week
- Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering☆55Updated 3 years ago
- A python based blade parametrization tool☆69Updated last year
- OpenFOAM case files for simulating NACA foils.☆57Updated 7 months ago