montagdude / Xoptfoil

Related projects: ⓘ

• DARcorporation / xfoil-python
  Stripped down version of XFOIL as compiled python module
  ☆87Updated 3 years ago
• cfsengineering / CEASIOMpy
  CEASIOMpy is a Python conceptual aircraft design environment
  ☆70Updated 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…
  ☆68Updated 4 months ago
• airinnova / pytornado
  An implementation of the vortex-lattice method (VLM)
  ☆25Updated last year
• aqreed / PyVLM
  Vortex Lattice Method library written in Python
  ☆41Updated 4 years ago
• pointwise / VSP2CFD
  Generate volume meshes for OpenVSP generated surface meshes.
  ☆25Updated 3 years ago
• usuaero / AirfoilDatabase
  A Python module for modeling airfoils
  ☆29Updated 9 months ago
• kegiljarhus / pyBEMT
  Implementation of the Blade Element Momentum Theory for turbines and propellers in Python
  ☆57Updated last year
• mdolab / CMPLXFOIL
  ☆29Updated 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…
  ☆61Updated 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…
  ☆38Updated 7 years ago
• usuaero / panairwrapper
  A python wrapper of the Panair/A502 panel code.
  ☆14Updated 2 years ago
• DARcorporation / xrotor-python
  Stripped down version of XROTOR as compiled python module
  ☆16Updated last year
• helloDestroyerOfWorlds / propeller_design_tools
  ☆20Updated this week
• pedrosecchi67 / LovelacePM
  Open source, python-interpretable vortex panel method design to optimize aircraft configuration studies
  ☆38Updated 4 years ago
• byuflowlab / FLOWVLM
  Vortex lattice method for inviscid lifting-surface aerodynamics
  ☆38Updated last month
• SaTa999 / pyPanair
  A pre/post processor for PANAIR
  ☆13Updated 3 years ago
• usuaero / PyPan
  A panel-based flow solver. Currently in beta but with working solvers for incompressible and inviscid hypersonic flow.
  ☆18Updated 2 years ago
• airinnova / airfoils
  Object-oriented airfoils (aerofoils) for Python
  ☆31Updated last year
• mdolab / OpenAeroStruct
  OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.
  ☆192Updated last month
• dgorissen / naca
  Generate 4 and 5 digit NACA airfoil sections
  ☆34Updated 2 years ago
• DLR-SL / CPACS
  CPACS - Common Parametric Aircraft Configuration Schema
  ☆79Updated 2 weeks ago
• fast-aircraft-design / FAST-OAD
  FAST-OAD: An open source framework for rapid Overall Aircraft Design
  ☆48Updated this week
• byuflowlab / CCBlade.jl
  Blade Element Momentum Method for Propellers and Turbines
  ☆56Updated last week
• OpenMDAO / mphys
  Multiphysics with OpenMDAO
  ☆47Updated last month
• pointwise / AircraftMesher
  A Glyph script demonstrating how to automate viscous meshing for aircraft geometry.
  ☆22Updated 3 years ago
• DLR-AE / PanelAero
  An Implementation of the Vortex Lattice (VLM) and the Doublet Lattice Method (DLM) for aeroelasticity.
  ☆17Updated 2 weeks ago
• smdogroup / tacs
  Finite-element library for analysis and adjoint-based gradient evaluation
  ☆102Updated this week
• usuaero / MachUpX
  Fast and accurate aerodynamic modeling using general numerical lifting-line theory.
  ☆92Updated 3 months ago
• montagdude / libxfoil
  2-dimensional airfoil aerodynamics library
  ☆12Updated last year