sobester / ADRpyLinks
Aircraft Design Recipes in Python
☆115Updated last year
Alternatives and similar repositories for ADRpy
Users that are interested in ADRpy are comparing it to the libraries listed below
Sorting:
- Fast and accurate aerodynamic modeling using general numerical lifting-line theory.☆111Updated last year
- CEASIOMpy is a Python conceptual aircraft design environment☆110Updated this week
- xflrpy is a python enabled version of xflr5 for scripting and design optimization.☆62Updated 4 months ago
- OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.☆220Updated 2 weeks ago
- NASA's aircraft analysis, design, and optimization tool☆194Updated last week
- FAST-OAD: An open source framework for rapid Overall Aircraft Design☆66Updated last week
- ☆46Updated 5 months ago
- An Aircraft Design Toolbox☆443Updated last year
- Vortex Lattice Method library written in Python☆41Updated 5 years ago
- ☆87Updated 6 months ago
- Stripped down version of XFOIL as compiled python module☆99Updated 4 years ago
- OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures☆44Updated 2 weeks ago
- A fully-featured flight simulator, capable of real-time lifting-line aerodynamic modelling.☆54Updated 3 years ago
- The ultimate electric propulsion modeling and optimization module.☆22Updated 4 years ago
- Matlab code to accompany "Aircraft Aerodynamic Design: Geometry and Optimization" by Sobester and Forrester (2015)☆17Updated 6 years ago
- Future Aircraft Sizing Tool☆86Updated this week
- An interactional aerodynamics and acoustics solver for multirotor aircraft and wind energy☆301Updated last week
- This is where the tutorial scripts live☆24Updated 3 years ago
- A Matlab tool to visualize recorded or simulated flight data☆163Updated last month
- Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code☆157Updated 3 weeks ago
- NeuralFoil is a practical airfoil aerodynamics analysis tool using physics-informed machine learning, in pure Python/NumPy.☆251Updated last month
- A python interface for DATCOM. Provides export/ parsing capabilities.☆27Updated 12 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
- CPACS - Common Parametric Aircraft Configuration Schema☆87Updated last month
- An implementation of the vortex-lattice method (VLM)☆34Updated last year
- FAST-(OAD)-GA is a framework for performing rapid Overall Aircraft Design for General Aviation Aircraft☆36Updated last week
- MACH: MDO of Aircraft Configurations with High fidelity☆132Updated last month
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python☆68Updated 2 years ago
- Blade Element Momentum Method for Propellers and Turbines☆69Updated last week
- 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…☆71Updated 4 years ago