Alternatives and similar repositories for AirfoilEditor

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

• mdolab / CMPLXFOIL
  ☆39Updated 5 months ago
• DARcorporation / xfoil-python
  Stripped down version of XFOIL as compiled python module
  ☆103Updated 4 years ago
• Mikekiely / wuFoil
  An all in one airfoil modelling, meshing, analysis, and optimization tool with built in support for gmsh, SU2, and xfoil
  ☆36Updated 2 months 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…
  ☆48Updated 8 years ago
• 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…
  ☆73Updated 4 years ago
• drarahimi / AERO_Console
  This is a graphical user interface for Mark Drela's Athena Vortex Lattice (AVL) and XFoil
  ☆12Updated 6 months ago
• kegiljarhus / pyBEMT
  Implementation of the Blade Element Momentum Theory for turbines and propellers in Python
  ☆70Updated 2 years ago
• m-selig / PROFOIL
  PROFOIL for inverse airfoil design
  ☆32Updated 10 months ago
• airinnova / pytornado
  An implementation of the vortex-lattice method (VLM)
  ☆36Updated 2 years ago
• usuaero / AirfoilDatabase
  A Python module for modeling airfoils
  ☆39Updated last year
• jxjo / Xoptfoil2
  The Airfoil Optimizer
  ☆16Updated last week
• usuaero / MachLine
  A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.
  ☆45Updated 6 months ago
• DARcorporation / xrotor-python
  Stripped down version of XROTOR as compiled python module
  ☆22Updated 2 years ago
• cfsengineering / CEASIOMpy
  CEASIOMpy is a Python conceptual aircraft design environment
  ☆116Updated this week
• OpenMDAO / pyCycle
  Thermodynamic cycle modeling library, built on top of OpenMDAO
  ☆126Updated last month
• dqsis / parsec-airfoils
  Generate and plot the contour of an airfoil using the PARSEC parameterization
  ☆17Updated 10 years ago
• Matthias231 / The-Strak-Machine
  Create airfoils for a wing using the airfoil optimizer Xoptfoil-JX
  ☆12Updated 2 years ago
• mdolab / OpenAeroStruct
  OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.
  ☆227Updated last week
• fast-aircraft-design / FAST-OAD
  FAST-OAD: An open source framework for rapid Overall Aircraft Design
  ☆69Updated last week
• DLR-AE / PanelAero
  An Implementation of the Vortex Lattice (VLM) and the Doublet Lattice Method (DLM) for aeroelasticity.
  ☆34Updated this week
• booya-at / parabem
  2d and 3d panelmethod to compute potential flow
  ☆15Updated 7 months ago
• aqreed / PyVLM
  Vortex Lattice Method library written in Python
  ☆42Updated 5 years ago
• OpenMDAO / mphys
  Multiphysics with OpenMDAO
  ☆109Updated last month
• dgorissen / naca
  Generate 4 and 5 digit NACA airfoil sections
  ☆40Updated 11 months ago
• NAnand-TUD / parablade
  A python based blade parametrization tool
  ☆63Updated last year
• OpenOrion / parafoil
  the open source parametric airfoil generator
  ☆30Updated 10 months ago
• SaTa999 / pyPanair
  A pre/post processor for PANAIR
  ☆17Updated 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…
  ☆40Updated 10 months ago
• byuflowlab / DuctAPE.jl
  Ducted Axisymmetric Propulsor Evaluation
  ☆13Updated last week
• mdolab / MACH-Aero
  MACH: MDO of Aircraft Configurations with High fidelity
  ☆136Updated this week