jxjo / AirfoilEditorLinks
Airfoil Editor to view, edit airfoils
☆27Updated this week
Alternatives and similar repositories for AirfoilEditor
Users that are interested in AirfoilEditor are comparing it to the libraries listed below
Sorting:
- ☆38Updated last month
- An all in one airfoil modelling, meshing, analysis, and optimization tool with built in support for gmsh, SU2, and xfoil☆41Updated 6 months 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
- Stripped down version of XROTOR as compiled python module☆24Updated 2 years ago
- PROFOIL for inverse airfoil design☆35Updated last year
- The Airfoil Optimizer☆21Updated this week
- Stripped down version of XFOIL as compiled python module☆108Updated 4 years ago
- 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
- A Python module for modeling airfoils☆41Updated 2 years ago
- FAST-OAD: An open source framework for rapid Overall Aircraft Design☆76Updated last month
- This is a graphical user interface for Mark Drela's Athena Vortex Lattice (AVL) and XFoil☆15Updated 2 weeks ago
- Open source, python-interpretable vortex panel method design to optimize aircraft configuration studies☆41Updated 5 years ago
- A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.☆46Updated 10 months ago
- Generate 4 and 5 digit NACA airfoil sections☆41Updated last year
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python☆80Updated 3 years ago
- A pre/post processor for PANAIR☆20Updated 4 years ago
- Generate and plot the contour of an airfoil using the PARSEC parameterization☆18Updated 10 years ago
- Create airfoils for a wing using the airfoil optimizer Xoptfoil-JX☆12Updated 2 years ago
- BladeX - Python Blade Morphing☆83Updated last week
- OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.☆241Updated 3 months ago
- Object-oriented airfoils (aerofoils) for Python☆39Updated 2 years ago
- An implementation of the vortex-lattice method (VLM)☆38Updated 2 years ago
- 2d and 3d panelmethod to compute potential flow☆17Updated last year
- CPACS - Common Parametric Aircraft Configuration Schema☆97Updated 2 months ago
- Blade Element Momentum Method for Propellers and Turbines☆75Updated last month
- A tool to manipulate control points of bezier curves. Main intended use is to generate .dat airfoil files which can be used to design sub…☆17Updated last year
- Thermodynamic cycle modeling library, built on top of OpenMDAO☆147Updated 2 months ago
- Differentiable and scalable 3D aerodynamics, (optionally) on the GPU.☆10Updated 9 months ago
- Vortex Lattice Method library written in Python☆44Updated 6 years ago
- A python based blade parametrization tool☆67Updated last year