supaero-aircraft-design / FAST-GALinks
FAST-(OAD)-GA is a framework for performing rapid Overall Aircraft Design for General Aviation Aircraft
☆37Updated this week
Alternatives and similar repositories for FAST-GA
Users that are interested in FAST-GA are comparing it to the libraries listed below
Sorting:
- FAST-OAD: An open source framework for rapid Overall Aircraft Design☆76Updated 2 weeks ago
- OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures☆53Updated last month
- A pre/post processor for PANAIR☆19Updated 4 years ago
- Future Aircraft Sizing Tool☆107Updated last week
- Computational Aerodynamics Lab☆30Updated 5 years ago
- Aircraft Design, Analysis and Optimization Code☆25Updated this week
- An implementation of the vortex-lattice method (VLM)☆38Updated 2 years ago
- CEASIOMpy is a Python conceptual aircraft design environment☆134Updated this week
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python☆80Updated 3 years ago
- Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering☆55Updated 3 years ago
- OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.☆239Updated 2 months ago
- Matlab code to accompany "Aircraft Aerodynamic Design: Geometry and Optimization" by Sobester and Forrester (2015)☆20Updated 6 years ago
- Codes related to the analysis, design, and optimization of on-demand, electric vertical-takeoff-and-landing aircraft. A preprint of an up…☆44Updated 5 years ago
- A panel-based flow solver. Currently in beta but with working solvers for incompressible and inviscid hypersonic flow.☆21Updated 3 years ago
- Blade Element Momentum Theory Function for MATLAB☆12Updated 7 years ago
- A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.☆45Updated 9 months ago
- Vortex Lattice Method library written in Python☆44Updated 6 years ago
- A MATLAB GUI for estimating some properties of turbines, the code is mainly based on Mattingly's "Elements of Propulsion". This repositor…☆22Updated 8 years ago
- Stripped down version of XFOIL as compiled python module☆105Updated 4 years ago
- Aeroelastic Aircraft Design and Simulation Tool☆29Updated 7 years ago
- Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code☆170Updated 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
- A python library for generating PDF XDSM diagrams.☆71Updated 3 months ago
- A python interface for DATCOM. Provides export/ parsing capabilities.☆28Updated 13 years ago
- NASA's aircraft analysis, design, and optimization tool☆241Updated this week
- This is where the tutorial scripts live☆26Updated 3 years ago
- CPACS - Common Parametric Aircraft Configuration Schema☆97Updated 2 months ago
- Thermodynamic cycle modeling library, built on top of OpenMDAO☆143Updated 2 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…☆75Updated 4 years ago
- OpenMDAO solvers and drivers to handle specific methods.☆12Updated 2 months ago