Alternatives and similar repositories for PyAero:

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

• mdolab / MACH-Aero
  MACH: MDO of Aircraft Configurations with High fidelity
  ☆125Updated last month
• cfsengineering / CEASIOMpy
  CEASIOMpy is a Python conceptual aircraft design environment
  ☆88Updated this week
• mdolab / OpenAeroStruct
  OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.
  ☆205Updated last week
• mdolab / dafoam
  DAFoam: Discrete Adjoint with OpenFOAM for High-fidelity Multidisciplinary Design Optimization
  ☆247Updated this week
• 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
• OpenMDAO / mphys
  Multiphysics with OpenMDAO
  ☆98Updated this week
• peterdsharpe / NeuralFoil
  NeuralFoil is a practical airfoil aerodynamics analysis tool using physics-informed machine learning, in pure Python/NumPy.
  ☆182Updated this week
• nextfoam / baram
  CFD for Everyone
  ☆119Updated last month
• mdolab / adflow
  ADflow is a finite volume RANS solver tailored for gradient-based aerodynamic design optimization.
  ☆253Updated 3 weeks ago
• usuaero / AirfoilDatabase
  A Python module for modeling airfoils
  ☆35Updated last year
• ImperialCollegeLondon / sharpy
  Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code
  ☆131Updated this week
• DARcorporation / xfoil-python
  Stripped down version of XFOIL as compiled python module
  ☆94Updated 3 years ago
• smdogroup / tacs
  Finite-element library for analysis and adjoint-based gradient evaluation
  ☆115Updated last week
• cotri / BEMT
  Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering
  ☆42Updated 2 years ago
• nasa / pyturbo-aero
  Turbomachinery Blade and Flow path design tool
  ☆38Updated this week
• usuaero / MachUpX
  Fast and accurate aerodynamic modeling using general numerical lifting-line theory.
  ☆108Updated 10 months ago
• byuflowlab / FLOWUnsteady
  An interactional aerodynamics and acoustics solver for multirotor aircraft and wind energy
  ☆283Updated this week
• sobester / ADRpy
  Aircraft Design Recipes in Python
  ☆110Updated 11 months ago
• OpenMDAO / pyCycle
  Thermodynamic cycle modeling library, built on top of OpenMDAO
  ☆91Updated 2 weeks ago
• 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
• kegiljarhus / pyBEMT
  Implementation of the Blade Element Momentum Theory for turbines and propellers in Python
  ☆63Updated 2 years ago
• nasa / CFL3D
  ☆292Updated 2 years ago
• petebachant / NACAFoil-OpenFOAM
  OpenFOAM case files for simulating NACA foils.
  ☆49Updated last month
• 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
• byuflowlab / CCBlade.jl
  Blade Element Momentum Method for Propellers and Turbines
  ☆65Updated last month
• mathLab / BladeX
  BladeX - Python Blade Morphing
  ☆73Updated last week
• aqreed / PyVLM
  Vortex Lattice Method library written in Python
  ☆41Updated 5 years ago
• hystrath / hyStrath
  Hypersonic / Rarefied gas dynamics code developments (GPL-3.0)
  ☆233Updated last year
• mdolab / pygeo
  pyGeo provides geometric design variables and constraints suitable for gradient-based optimization.
  ☆148Updated this week
• jte0419 / Panel_Methods
  Source and vortex panel method codes referenced in my YouTube videos.
  ☆93Updated 4 years ago