fast-aircraft-design / FAST-OADLinks
FAST-OAD: An open source framework for rapid Overall Aircraft Design
☆65Updated 2 weeks ago
Alternatives and similar repositories for FAST-OAD
Users that are interested in FAST-OAD are comparing it to the libraries listed below
Sorting:
- CEASIOMpy is a Python conceptual aircraft design environment☆107Updated this week
- Blade Element Momentum Method for Propellers and Turbines☆67Updated last month
- FAST-(OAD)-GA is a framework for performing rapid Overall Aircraft Design for General Aviation Aircraft☆35Updated this week
- Multiphysics with OpenMDAO☆105Updated 3 weeks ago
- OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures☆42Updated last month
- OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.☆216Updated last month
- OpenMDAO solvers and drivers to handle specific methods.☆12Updated 2 months ago
- Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code☆157Updated 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…☆23Updated 4 months ago
- A python library for generating PDF XDSM diagrams.☆64Updated 3 months ago
- ☆37Updated 2 months ago
- OpenMDAO 2020 Reverse Hackathon☆14Updated 9 months 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…☆71Updated 4 years ago
- ☆12Updated 4 months ago
- Stripped down version of XFOIL as compiled python module☆99Updated 3 years ago
- NASA's aircraft analysis, design, and optimization tool☆191Updated this week
- 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
- Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering☆45Updated 2 years ago
- Vortex Lattice Method library written in Python☆41Updated 5 years ago
- Thermodynamic cycle modeling library, built on top of OpenMDAO☆108Updated last week
- CPACS - Common Parametric Aircraft Configuration Schema☆86Updated last month
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python