kjayawar / PROFOIL-UILinks
Simple GUI for PROFOIL
☆17Updated 9 months ago
Alternatives and similar repositories for PROFOIL-UI
Users that are interested in PROFOIL-UI are comparing it to the libraries listed below
Sorting:
- This is a graphical user interface for Mark Drela's Athena Vortex Lattice (AVL) and XFoil☆12Updated 4 months ago
- PROFOIL for inverse airfoil design☆31Updated 9 months ago
- An object-oriented Python 3 GUI and API for single- and multi-element parametric airfoil design, analysis, and optimization☆19Updated 2 weeks ago
- A pre/post processor for PANAIR☆16Updated 4 years ago
- ☆39Updated 4 months 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…☆12Updated last year
- LOw Reynolds number Aircraft Analysis with Xfoil☆14Updated 5 years ago
- A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.☆44Updated 4 months ago
- A Python module for modeling airfoils☆37Updated last year
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python☆69Updated 2 years ago
- Airfoil optimization with Xfoil☆53Updated 3 years ago
- An all in one airfoil modelling, meshing, analysis, and optimization tool with built in support for gmsh, SU2, and xfoil☆36Updated last month
- A python wrapper of the Panair/A502 panel code.☆18Updated 3 years ago
- ☆25Updated 12 years ago
- Stripped down version of XFOIL as compiled python module☆99Updated 4 years ago
- An implementation of the vortex-lattice method (VLM)☆34Updated 2 years ago
- MYSTRAN is a general purpose finite element analysis solver☆62Updated 2 years ago
- MACH: MDO of Aircraft Configurations with High fidelity☆134Updated 2 months ago
- Generate and plot the contour of an airfoil using the PARSEC parameterization☆17Updated 10 years ago
- All updates to this code are to get NASTRAN-95 running in a GNU environment. It even runs on a Raspberry Pi! Some recent changes to the …☆35Updated 5 years ago
- CEASIOMpy is a Python conceptual aircraft design environment☆112Updated this week
- Adaptable framework for aerothermoelastic analysis and adjoint-based gradient evaluation☆33Updated 3 weeks ago
- Unsteady Vortex Lattice Method for Aeroelasticity in C++☆26Updated last month
- Multiphysics with OpenMDAO☆106Updated 2 months ago
- 2-dimensional airfoil aerodynamics library☆13Updated 2 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…☆46Updated 7 years ago
- Object-oriented airfoils (aerofoils) for Python☆37Updated 2 years ago
- A python based blade parametrization tool☆61Updated 11 months ago
- Finite-element library for analysis and adjoint-based gradient evaluation☆129Updated 2 weeks ago
- Weissinger-L linear aerodynamic method implemented in Python☆9Updated last year