Alternatives and similar repositories for libxfoil

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

• dqsis / parsec-airfoils
  Generate and plot the contour of an airfoil using the PARSEC parameterization
  ☆17Updated 10 years ago
• ImperialCollegeLondon / flexibleaircraftbook
  Scripts for Dynamics of Flexible Aircraft
  ☆20Updated 2 months ago
• mdolab / CMPLXFOIL
  ☆37Updated 2 months ago
• mdolab / AerostructuralOptBenchmark
  ☆12Updated 4 months ago
• booya-at / parabem
  2d and 3d panelmethod to compute potential flow
  ☆14Updated 5 months ago
• ACea15 / FENIAX
  ☆20Updated this week
• byuflowlab / DuctAPE.jl
  Ducted Axisymmetric Propulsor Evaluation
  ☆13Updated this week
• Mikekiely / wuFoil
  An all in one airfoil modelling, meshing, analysis, and optimization tool with built in support for gmsh, SU2, and xfoil
  ☆32Updated last month
• DARcorporation / xfoil-python
  Stripped down version of XFOIL as compiled python module
  ☆99Updated 3 years 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…
  ☆46Updated 7 years ago
• cfsengineering / CEASIOMpy
  CEASIOMpy is a Python conceptual aircraft design environment
  ☆107Updated 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
• usuaero / panairwrapper
  A python wrapper of the Panair/A502 panel code.
  ☆17Updated 2 years ago
• airinnova / pytornado
  An implementation of the vortex-lattice method (VLM)
  ☆32Updated last year
• pedrosecchi67 / LovelacePM
  Open source, python-interpretable vortex panel method design to optimize aircraft configuration studies
  ☆37Updated 5 years ago
• SaTa999 / pyPanair
  A pre/post processor for PANAIR
  ☆15Updated 4 years ago
• ImperialCollegeLondon / UVLM
  Unsteady Vortex Lattice Method for Aeroelasticity in C++
  ☆25Updated this week
• OpenMDAO / mphys
  Multiphysics with OpenMDAO
  ☆105Updated last month
• kegiljarhus / pyBEMT
  Implementation of the Blade Element Momentum Theory for turbines and propellers in Python
  ☆68Updated 2 years ago
• montagdude / loraax
  LOw Reynolds number Aircraft Analysis with Xfoil
  ☆14Updated 4 years ago
• daniel-de-vries / xfoil-python
  Stripped down version of XFOIL as compiled python module
  ☆21Updated 4 years ago
• DARcorporation / xrotor-python
  Stripped down version of XROTOR as compiled python module
  ☆22Updated 2 years ago
• usuaero / MachLine
  A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.
  ☆41Updated 3 months 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.
  ☆33Updated 9 months ago
• NAnand-TUD / parablade
  A python based blade parametrization tool
  ☆55Updated 9 months ago
• mdolab / MACH-Aero
  MACH: MDO of Aircraft Configurations with High fidelity
  ☆131Updated 3 weeks ago
• cotri / BEMT
  Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering
  ☆45Updated 2 years ago
• usuaero / PyPan
  A panel-based flow solver. Currently in beta but with working solvers for incompressible and inviscid hypersonic flow.
  ☆19Updated 3 years ago
• byuflowlab / CCBlade.jl
  Blade Element Momentum Method for Propellers and Turbines
  ☆67Updated last month