Alternatives and similar repositories for PyXFLR:

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

• nikhil-sethi / xflrpy
  xflrpy is a python enabled version of xflr5 for scripting and design optimization.
  ☆58Updated last month
• fast-aircraft-design / FAST-OAD
  FAST-OAD: An open source framework for rapid Overall Aircraft Design
  ☆61Updated last week
• sobester / ADRpy
  Aircraft Design Recipes in Python
  ☆111Updated last year
• mdolab / OpenAeroStruct
  OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.
  ☆206Updated this week
• cfsengineering / CEASIOMpy
  CEASIOMpy is a Python conceptual aircraft design environment
  ☆94Updated this week
• ImperialCollegeLondon / sharpy
  Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code
  ☆147Updated 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 4 years ago
• rafaelpsilva07 / composipy
  composipy is a python library to calculate composite plates using the classical laminate theory. This library is designed to be simple, u…
  ☆37Updated 5 months ago
• DARcorporation / xfoil-python
  Stripped down version of XFOIL as compiled python module
  ☆94Updated 3 years ago
• byuflowlab / FLOWUnsteady
  An interactional aerodynamics and acoustics solver for multirotor aircraft and wind energy
  ☆287Updated 2 weeks ago
• kegiljarhus / pyBEMT
  Implementation of the Blade Element Momentum Theory for turbines and propellers in Python
  ☆63Updated 2 years ago
• OpenMDAO / Aviary
  NASA's aircraft analysis, design, and optimization tool
  ☆177Updated last week
• vtpasquale / VoLAre
  Vortex Lattice for Aeroelasticity
  ☆12Updated 7 years ago
• byuflowlab / CCBlade.jl
  Blade Element Momentum Method for Propellers and Turbines
  ☆65Updated last month
• usuaero / MachUpX
  Fast and accurate aerodynamic modeling using general numerical lifting-line theory.
  ☆108Updated 10 months ago
• suavecode / SUAVE
  An Aircraft Design Toolbox
  ☆431Updated last year
• OpenMDAO / pyCycle
  Thermodynamic cycle modeling library, built on top of OpenMDAO
  ☆91Updated last week
• vvflow / vvflow
  CFD software for performing flow simulations with Viscous Vortex Domains (VVD) method
  ☆116Updated 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 / MACH-Aero
  MACH: MDO of Aircraft Configurations with High fidelity
  ☆125Updated 2 months ago
• cadowd / proppy
  RC propeller and motor selection tool
  ☆11Updated 7 years ago
• peterdsharpe / NeuralFoil
  NeuralFoil is a practical airfoil aerodynamics analysis tool using physics-informed machine learning, in pure Python/NumPy.
  ☆188Updated last week
• cotri / BEMT
  Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering
  ☆43Updated 2 years ago
• OpenMDAO / mphys
  Multiphysics with OpenMDAO
  ☆98Updated last week
• vsdsantos / nastran-aeroelasticity
  Some usefull routines for aeroelastic analysis with NASTRAN.
  ☆19Updated 2 years ago
• mdolab / pyXDSM
  A python library for generating PDF XDSM diagrams.
  ☆61Updated last month
• aqreed / PyVLM
  Vortex Lattice Method library written in Python
  ☆41Updated 5 years ago
• mvernacc / proptools
  Rocket propulsion design calculation tools
  ☆48Updated 2 years ago
• polmes / xflr5-ubuntu
  How to install the latest XFLR5 version on Ubuntu Linux
  ☆34Updated last year
• OpenMDAO / POEMs
  Proposals for OpenMDAO Enhancements
  ☆16Updated last month