OpenMDAO / AviaryLinks
NASA's aircraft analysis, design, and optimization tool
☆241Updated last week
Alternatives and similar repositories for Aviary
Users that are interested in Aviary are comparing it to the libraries listed below
Sorting:
- OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.☆239Updated 2 months ago
- CEASIOMpy is a Python conceptual aircraft design environment☆134Updated this week
- Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code☆170Updated 3 weeks ago
- An interactional aerodynamics and acoustics solver for multirotor aircraft and wind energy☆336Updated 3 months ago
- OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures☆53Updated last month
- FAST-OAD: An open source framework for rapid Overall Aircraft Design☆76Updated 3 weeks ago
- NeuralFoil is a practical airfoil aerodynamics analysis tool using physics-informed machine learning, exposed to end-users in pure Python…☆342Updated 2 months ago
- Multiphysics with OpenMDAO☆113Updated last week
- An Aircraft Design Toolbox☆488Updated last year
- Thermodynamic cycle modeling library, built on top of OpenMDAO☆144Updated 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…☆76Updated 4 years ago
- MACH: MDO of Aircraft Configurations with High fidelity☆147Updated last month
- Stripped down version of XFOIL as compiled python module☆105Updated 4 years ago
- ADflow is a finite volume RANS solver tailored for gradient-based aerodynamic design optimization.☆290Updated 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…☆27Updated last week
- Blade Element Momentum Method for Propellers and Turbines☆74Updated last month
- A python library for generating PDF XDSM diagrams.☆71Updated 3 months ago
- Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering☆55Updated 3 years ago
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python☆80Updated 3 years ago
- DAFoam: Discrete Adjoint with OpenFOAM for High-fidelity Multidisciplinary Design Optimization☆300Updated last week
- PyAero is an open-source airfoil contour analysis and CFD meshing tool.☆225Updated 3 months ago
- Fast and accurate aerodynamic modeling using general numerical lifting-line theory.☆122Updated last year
- Turbomachinery Blade and Flow path design tool☆68Updated this week
- An implementation of the vortex-lattice method (VLM)☆38Updated 2 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
- CPACS - Common Parametric Aircraft Configuration Schema☆97Updated 2 months ago
- Future Aircraft Sizing Tool☆107Updated this week
- Python BEM solver for linear potential flow, based on Nemoh.☆196Updated last week
- Aircraft Design Recipes in Python☆127Updated last year
- conceptual design of vtol platforms☆18Updated 6 years ago