kjayawar / PROFOIL-UILinks
Simple GUI for PROFOIL
☆19Updated last year
Alternatives and similar repositories for PROFOIL-UI
Users that are interested in PROFOIL-UI are comparing it to the libraries listed below
Sorting:
- PROFOIL for inverse airfoil design☆35Updated last year
- An object-oriented Python 3 GUI and API for single- and multi-element parametric airfoil design, analysis, and optimization☆21Updated 4 months ago
- This is a graphical user interface for Mark Drela's Athena Vortex Lattice (AVL) and XFoil☆15Updated 2 weeks ago
- An all in one airfoil modelling, meshing, analysis, and optimization tool with built in support for gmsh, SU2, and xfoil☆41Updated 6 months ago
- ☆38Updated last month
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python☆80Updated 3 years ago
- MACH: MDO of Aircraft Configurations with High fidelity☆148Updated 2 months ago
- A pre/post processor for PANAIR☆20Updated 4 years ago
- Stripped down version of XFOIL as compiled python module☆108Updated 4 years ago
- 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
- A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.☆46Updated 10 months ago
- OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.☆241Updated 3 months ago
- Multiphysics with OpenMDAO☆115Updated 3 weeks ago
- An implementation of the vortex-lattice method (VLM)☆38Updated 2 years ago
- A Python module for modeling airfoils☆41Updated 2 years ago
- Airfoil optimization with Xfoil☆55Updated 3 years ago
- Stripped down version of XROTOR as compiled python module☆24Updated 2 years ago
- A python based blade parametrization tool☆67Updated last year
- CEASIOMpy is a Python conceptual aircraft design environment☆134Updated this week
- Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code☆169Updated this week
- Adaptable framework for aerothermoelastic analysis and adjoint-based gradient evaluation☆35Updated 2 months ago
- Finite-element library for analysis and adjoint-based gradient evaluation☆138Updated this week
- ezaero - Easy aerodynamics in Python☆33Updated 5 years ago
- Generate and plot the contour of an airfoil using the PARSEC parameterization☆18Updated 10 years ago
- A python wrapper of the Panair/A502 panel code.☆18Updated 3 years 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
- 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
- An Implementation of the Vortex Lattice (VLM) and the Doublet Lattice Method (DLM) for aeroelasticity.☆41Updated last month
- Field Panel Method for solving the Full Potential Equation☆12Updated 6 years ago
- OpenFOAM case files for simulating NACA foils.☆57Updated 7 months ago