adeharo9 / NACA-airfoil-generatorLinks
Airfoil generator of NACA 4, 5 and 6 Series
☆24Updated 7 years ago
Alternatives and similar repositories for NACA-airfoil-generator
Users that are interested in NACA-airfoil-generator are comparing it to the libraries listed below
Sorting:
- Vortex Lattice Method library written in Python☆42Updated 5 years ago
- FAST-OAD: An open source framework for rapid Overall Aircraft Design☆71Updated 2 weeks ago
- OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.☆232Updated this week
- An implementation of the vortex-lattice method (VLM)☆37Updated 2 years ago
- Stripped down version of XFOIL as compiled python module☆103Updated 4 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…☆48Updated 8 years ago
- CEASIOMpy is a Python conceptual aircraft design environment☆119Updated this week
- MACH: MDO of Aircraft Configurations with High fidelity☆139Updated this week
- Aircraft Design Recipes in Python☆121Updated last year
- A pre/post processor for PANAIR☆17Updated 4 years ago
- OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures☆48Updated last week
- Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering☆50Updated 3 years ago
- Some usefull routines for aeroelastic analysis with NASTRAN.☆20Updated 3 years ago
- conceptual design of vtol platforms☆16Updated 6 years ago
- ☆39Updated 2 weeks ago
- The Loads Kernel Software allows for the calculation of quasi-steady and dynamic maneuver loads, unsteady gust loads in the time and freq…☆26Updated 3 weeks ago
- Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code☆160Updated 2 weeks 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…☆73Updated 4 years ago
- A Python module for modeling airfoils☆39Updated last year
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python☆70Updated 2 years ago
- Multiphysics with OpenMDAO☆110Updated 2 weeks ago
- A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.☆45Updated 6 months ago
- Aeroelastic Aircraft Design and Simulation Tool☆29Updated 7 years ago
- Aeroelastic Composite Beam Analysis Tool☆19Updated 8 years ago
- A panel-based flow solver. Currently in beta but with working solvers for incompressible and inviscid hypersonic flow.☆20Updated 3 years ago
- Blade Element Momentum Method for Propellers and Turbines☆69Updated last month
- Tucan remains among the simplest and most user friendly programs for aerodynamics based on vortex lattice methods. This project is unique…☆78Updated last year
- Open source, python-interpretable vortex panel method design to optimize aircraft configuration studies☆39Updated 5 years ago
- The ultimate electric propulsion modeling and optimization module.☆24Updated 4 years ago
- Thermodynamic cycle modeling library, built on top of OpenMDAO☆127Updated last month