Alternatives and similar repositories for BladeX

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

• usuaero / MachUp
  Numerical Lifting-Line Algorithm
  ☆44Updated 6 years ago
• usuaero / MachUp_Py
  Python Version of MachUp (Numerical Lifting-Line Method)
  ☆18Updated 6 years ago
• usuaero / Optix
  Python Gradient-Based Optimization Tool
  ☆10Updated 3 years ago
• arktools / aircraft-datcom
  Modified USAF Aircraft DATCOM
  ☆20Updated 13 years ago
• clolsonus / madesigner
  Model Airplane Rapid Design Toolkit
  ☆23Updated last month
• pointwise / VSP2CFD
  Generate volume meshes for OpenVSP generated surface meshes.
  ☆27Updated 4 years ago
• usuaero / AirfoilDatabase
  A Python module for modeling airfoils
  ☆39Updated last year
• usuaero / MachUpX
  Fast and accurate aerodynamic modeling using general numerical lifting-line theory.
  ☆114Updated last year
• usuaero / MachLine
  A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.
  ☆44Updated 5 months ago
• montagdude / Xoptfoil
  Airfoil optimization with Xfoil
  ☆53Updated 3 years ago
• DARcorporation / xrotor-python
  Stripped down version of XROTOR as compiled python module
  ☆22Updated 2 years ago
• SaTa999 / pyPanair
  A pre/post processor for PANAIR
  ☆17Updated 4 years ago
• ImperialCollegeLondon / UVLM
  Unsteady Vortex Lattice Method for Aeroelasticity in C++
  ☆27Updated 2 months ago
• cibinjoseph / KatzPlotkin
  An archive of the programs provided by Joseph Katz and Allen Plotkin in their book Low-Speed Aerodynamics
  ☆17Updated last year
• usuaero / Pylot
  A fully-featured flight simulator, capable of real-time lifting-line aerodynamic modelling.
  ☆55Updated 3 years ago
• jdcasey / airfoil-utils
  utility scripts for working with coordinate files from the UIUC Airfoil Database: http://m-selig.ae.illinois.edu/ads/coord_database.html
  ☆22Updated 7 years ago
• rbunge / QuadAir
  A Matlab implementation of the Compact Vortex Lattice Method, used to calculate the aerodynamics of fixed-wing aircraft.
  ☆14Updated 11 years ago
• andreagalle / labcalaero-20
  Computational Aerodynamics Lab
  ☆26Updated 5 years ago
• suavecode / Tutorials
  This is where the tutorial scripts live
  ☆24Updated 3 years ago
• SebastianDeubler / DatcomXL
  DATCOM-XL is a transparent and easy to use aircraft aerodynamic derivative estimation tool.
  ☆11Updated last year
• montagdude / loraax
  LOw Reynolds number Aircraft Analysis with Xfoil
  ☆14Updated 5 years ago
• geoffreynyaga / Kenya-One-Project
  Aircraft Conceptual Design Software
  ☆33Updated 2 years ago
• aqreed / PyVLM
  Vortex Lattice Method library written in Python
  ☆42Updated 5 years ago
• usuaero / panairwrapper
  A python wrapper of the Panair/A502 panel code.
  ☆18Updated 3 years ago
• kooroshg1 / FUN3D
  ☆23Updated 6 years ago
• usuaero / PyPan
  A panel-based flow solver. Currently in beta but with working solvers for incompressible and inviscid hypersonic flow.
  ☆20Updated 3 years ago
• nasa / Three-Dimensional-Nozzle-Design-Code
  ☆54Updated 5 years ago
• nasa / TLNS3D
  ☆49Updated 7 years ago
• nasa / OpenVSP3Plugin
  ☆22Updated 7 years ago
• pointwise / AircraftMesher
  A Glyph script demonstrating how to automate viscous meshing for aircraft geometry.
  ☆23Updated 5 months ago