Alternatives and similar repositories for Aviary:

Users that are interested in Aviary are comparing it to the libraries listed below

• mdolab / OpenAeroStruct
  OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.
  ☆205Updated last week
• cfsengineering / CEASIOMpy
  CEASIOMpy is a Python conceptual aircraft design environment
  ☆88Updated this week
• fast-aircraft-design / FAST-OAD
  FAST-OAD: An open source framework for rapid Overall Aircraft Design
  ☆60Updated this week
• mdolab / openconcept
  OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures
  ☆40Updated 3 weeks ago
• peterdsharpe / NeuralFoil
  NeuralFoil is a practical airfoil aerodynamics analysis tool using physics-informed machine learning, in pure Python/NumPy.
  ☆182Updated this week
• OpenMDAO / mphys
  Multiphysics with OpenMDAO
  ☆98Updated this week
• byuflowlab / FLOWUnsteady
  An interactional aerodynamics and acoustics solver for multirotor aircraft and wind energy
  ☆283Updated this week
• ImperialCollegeLondon / sharpy
  Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code
  ☆131Updated this week
• mdolab / MACH-Aero
  MACH: MDO of Aircraft Configurations with High fidelity
  ☆125Updated last month
• byuflowlab / CCBlade.jl
  Blade Element Momentum Method for Propellers and Turbines
  ☆65Updated last month
• DARcorporation / xfoil-python
  Stripped down version of XFOIL as compiled python module
  ☆94Updated 3 years ago
• ideas-um / FAST
  Future Aircraft Sizing Tool
  ☆77Updated this week
• OpenMDAO / pyCycle
  Thermodynamic cycle modeling library, built on top of OpenMDAO
  ☆91Updated 3 weeks ago
• supaero-aircraft-design / FAST-GA
  FAST-(OAD)-GA is a framework for performing rapid Overall Aircraft Design for General Aviation Aircraft
  ☆33Updated last week
• The-Fonz / xfoil-optimization-toolbox
  The Python XFOIL optimization toolbox can be used to optimize airfoils for a specific operating range, and might be useful to you for its…
  ☆44Updated 7 years ago
• mdolab / pyXDSM
  A python library for generating PDF XDSM diagrams.
  ☆61Updated last month
• cotri / BEMT
  Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering
  ☆42Updated 2 years ago
• OpenMDAO / POEMs
  Proposals for OpenMDAO Enhancements
  ☆15Updated last month
• leal26 / AeroPy
  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 3 years ago
• nasa / pyturbo-aero
  Turbomachinery Blade and Flow path design tool
  ☆38Updated this week
• suavecode / SUAVE
  An Aircraft Design Toolbox
  ☆429Updated last year
• sobester / airgeobookcode_m
  Matlab code to accompany "Aircraft Aerodynamic Design: Geometry and Optimization" by Sobester and Forrester (2015)
  ☆16Updated 6 years ago
• kegiljarhus / pyBEMT
  Implementation of the Blade Element Momentum Theory for turbines and propellers in Python
  ☆63Updated 2 years ago
• DLR-AE / LoadsKernel
  The Loads Kernel Software allows for the calculation of quasi-steady and dynamic maneuver loads, unsteady gust loads in the time and freq…
  ☆19Updated last month
• sobester / ADRpy
  Aircraft Design Recipes in Python
  ☆110Updated 11 months ago
• DLR-SL / CPACS
  CPACS - Common Parametric Aircraft Configuration Schema
  ☆82Updated 2 weeks ago
• aqreed / PyVLM
  Vortex Lattice Method library written in Python
  ☆41Updated 5 years ago
• DLR-AE / PanelAero
  An Implementation of the Vortex Lattice (VLM) and the Doublet Lattice Method (DLM) for aeroelasticity.
  ☆28Updated 6 months ago
• OpenVOGEL / Tucan
  Tucan remains among the simplest and most user friendly programs for aerodynamics based on vortex lattice methods. This project is unique…
  ☆73Updated 10 months ago
• usuaero / MachUpX
  Fast and accurate aerodynamic modeling using general numerical lifting-line theory.
  ☆108Updated 10 months ago