fast-aircraft-design / FAST-OADLinks
FAST-OAD: An open source framework for rapid Overall Aircraft Design
☆76Updated this week
Alternatives and similar repositories for FAST-OAD
Users that are interested in FAST-OAD are comparing it to the libraries listed below
Sorting:
- Blade Element Momentum Method for Propellers and Turbines☆72Updated last week
- OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures☆52Updated last month
- CEASIOMpy is a Python conceptual aircraft design environment☆133Updated last week
- OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.☆239Updated 2 months ago
- Stripped down version of XFOIL as compiled python module☆105Updated 4 years ago
- A python library for generating PDF XDSM diagrams.☆71Updated 3 months ago
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python☆77Updated 3 years ago
- Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code☆169Updated this week
- Multiphysics with OpenMDAO☆113Updated 2 weeks 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
- Thermodynamic cycle modeling library, built on top of OpenMDAO☆140Updated last month
- FAST-(OAD)-GA is a framework for performing rapid Overall Aircraft Design for General Aviation Aircraft☆36Updated last week
- Vortex Lattice Method library written in Python☆43Updated 6 years ago
- ☆38Updated this week
- The Loads Kernel Software allows for the calculation of quasi-steady and dynamic maneuver loads, unsteady gust loads in the time and freq…☆27Updated last week
- NASA's aircraft analysis, design, and optimization tool☆237Updated last week
- An implementation of the vortex-lattice method (VLM)☆38Updated 2 years ago
- Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering☆53Updated 3 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…☆74Updated 4 years ago
- An interactional aerodynamics and acoustics solver for multirotor aircraft and wind energy☆335Updated 3 months ago
- OpenMDAO solvers and drivers to handle specific methods.☆12Updated 2 months ago
- MACH: MDO of Aircraft Configurations with High fidelity☆145Updated last month
- A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.☆45Updated 9 months ago
- CPACS - Common Parametric Aircraft Configuration Schema☆97Updated last month
- Stripped down version of XROTOR as compiled python module☆23Updated 2 years ago
- A pre/post processor for PANAIR☆18Updated 4 years ago
- A blade element momentum method for analyzing wind turbine aerodynamic performance that is robust (guaranteed convergence), fast (superli…☆58Updated 4 months ago
- Open source, python-interpretable vortex panel method design to optimize aircraft configuration studies☆40Updated 5 years ago
- An all in one airfoil modelling, meshing, analysis, and optimization tool with built in support for gmsh, SU2, and xfoil☆39Updated 5 months ago
- ☆23Updated last month