Matthias231 / The-Strak-MachineLinks
Create airfoils for a wing using the airfoil optimizer Xoptfoil-JX
☆12Updated 2 years ago
Alternatives and similar repositories for The-Strak-Machine
Users that are interested in The-Strak-Machine are comparing it to the libraries listed below
Sorting:
- Airfoil Editor to view, edit airfoils☆23Updated last week
- xflrpy is a python enabled version of xflr5 for scripting and design optimization.☆72Updated last week
- Simple GUI for PROFOIL☆18Updated last year
- CPACS - Common Parametric Aircraft Configuration Schema☆95Updated last month
- 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
- This is a graphical user interface for Mark Drela's Athena Vortex Lattice (AVL) and XFoil☆14Updated 7 months ago
- The Airfoil Optimizer☆19Updated 2 weeks ago
- Airfoil optimization with Xfoil☆53Updated 3 years ago
- Xoptfoil-JX - modified version☆15Updated last year
- Generate and plot the contour of an airfoil using the PARSEC parameterization☆17Updated 10 years ago
- Stripped down version of XFOIL as compiled python module☆104Updated 4 years ago
- ezaero - Easy aerodynamics in Python☆33Updated 4 years ago
- A fun, lightweight tool to visualize potential flows quickly!☆19Updated 8 months ago
- OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.☆235Updated last week
- A pre/post processor for PANAIR☆17Updated 4 years ago
- This repository contains code development for the 4th credit project for AE416. The aim of the project is to compare different optimizati…☆25Updated 8 years ago
- 2d and 3d panelmethod to compute potential flow☆16Updated 9 months 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…☆74Updated 4 years ago
- An implementation of the vortex-lattice method (VLM)☆38Updated 2 years ago
- CEASIOMpy is a Python conceptual aircraft design environment☆121Updated this week
- LOw Reynolds number Aircraft Analysis with Xfoil☆14Updated 5 years ago
- A Python module for modeling airfoils☆39Updated last year
- ☆39Updated last month
- 2-dimensional airfoil aerodynamics library☆13Updated 2 years ago
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python☆71Updated 2 years ago
- Object-oriented airfoils (aerofoils) for Python☆38Updated 2 years ago
- PROFOIL for inverse airfoil design☆34Updated last year
- MACH: MDO of Aircraft Configurations with High fidelity☆141Updated last week
- Blade Element Method implementation for propeller calculations.☆14Updated 10 months ago
- Aircraft Configuration through Integrated Cross-disciplinary Scripting, Python package built on PythonOCC☆16Updated 7 years ago