Alternatives and similar repositories for OpenAeroStruct

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

• cfsengineering / CEASIOMpy
  CEASIOMpy is a Python conceptual aircraft design environment
  ☆107Updated this week
• ImperialCollegeLondon / sharpy
  Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code
  ☆156Updated last week
• mdolab / MACH-Aero
  MACH: MDO of Aircraft Configurations with High fidelity
  ☆131Updated 2 weeks ago
• OpenMDAO / mphys
  Multiphysics with OpenMDAO
  ☆105Updated 3 weeks ago
• OpenMDAO / Aviary
  NASA's aircraft analysis, design, and optimization tool
  ☆188Updated this week
• DARcorporation / xfoil-python
  Stripped down version of XFOIL as compiled python module
  ☆99Updated 3 years ago
• OpenMDAO / pyCycle
  Thermodynamic cycle modeling library, built on top of OpenMDAO
  ☆108Updated last week
• OpenVOGEL / Tucan
  Tucan remains among the simplest and most user friendly programs for aerodynamics based on vortex lattice methods. This project is unique…
  ☆75Updated last year
• mdolab / dafoam
  DAFoam: Discrete Adjoint with OpenFOAM for High-fidelity Multidisciplinary Design Optimization
  ☆264Updated last week
• mdolab / adflow
  ADflow is a finite volume RANS solver tailored for gradient-based aerodynamic design optimization.
  ☆262Updated 2 weeks ago
• fast-aircraft-design / FAST-OAD
  FAST-OAD: An open source framework for rapid Overall Aircraft Design
  ☆65Updated last week
• byuflowlab / CCBlade.jl
  Blade Element Momentum Method for Propellers and Turbines
  ☆67Updated 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 4 years ago
• byuflowlab / FLOWUnsteady
  An interactional aerodynamics and acoustics solver for multirotor aircraft and wind energy
  ☆294Updated 2 months ago
• chiefenne / PyAero
  PyAero is an open-source airfoil contour analysis and CFD meshing tool.
  ☆198Updated 5 months ago
• mdolab / openconcept
  OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures
  ☆42Updated last month
• 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…
  ☆46Updated 7 years ago
• mdolab / pyXDSM
  A python library for generating PDF XDSM diagrams.
  ☆64Updated 3 months ago
• DLR-SL / CPACS
  CPACS - Common Parametric Aircraft Configuration Schema
  ☆86Updated 3 weeks ago
• usuaero / MachUpX
  Fast and accurate aerodynamic modeling using general numerical lifting-line theory.
  ☆111Updated last year
• mdolab / pygeo
  pyGeo provides geometric design variables and constraints suitable for gradient-based optimization.
  ☆167Updated 3 weeks ago
• hystrath / hyStrath
  Hypersonic / Rarefied gas dynamics code developments (GPL-3.0)
  ☆242Updated last year
• nasa / pyturbo-aero
  Turbomachinery Blade and Flow path design tool
  ☆47Updated this week
• smdogroup / tacs
  Finite-element library for analysis and adjoint-based gradient evaluation
  ☆121Updated last week
• peterdsharpe / NeuralFoil
  NeuralFoil is a practical airfoil aerodynamics analysis tool using physics-informed machine learning, in pure Python/NumPy.
  ☆243Updated 2 weeks ago
• airinnova / pytornado
  An implementation of the vortex-lattice method (VLM)
  ☆32Updated last year
• 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…
  ☆22Updated 4 months ago
• cotri / BEMT
  Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering
  ☆45Updated 2 years ago
• kegiljarhus / pyBEMT
  Implementation of the Blade Element Momentum Theory for turbines and propellers in Python
  ☆68Updated 2 years ago
• mdolab / CMPLXFOIL
  ☆37Updated 2 months ago