Alternatives and similar repositories for pyXDSM:

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

• OpenMDAO / mphys
  Multiphysics with OpenMDAO
  ☆99Updated last week
• byuflowlab / CCBlade.jl
  Blade Element Momentum Method for Propellers and Turbines
  ☆65Updated last week
• OpenMDAO / pyCycle
  Thermodynamic cycle modeling library, built on top of OpenMDAO
  ☆96Updated 2 weeks ago
• DARcorporation / xfoil-python
  Stripped down version of XFOIL as compiled python module
  ☆96Updated 3 years ago
• fast-aircraft-design / FAST-OAD
  FAST-OAD: An open source framework for rapid Overall Aircraft Design
  ☆61Updated this week
• ImperialCollegeLondon / sharpy
  Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code
  ☆151Updated this week
• mdolab / openconcept
  OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures
  ☆40Updated this 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 / OpenAeroStruct
  OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.
  ☆209Updated last 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
• whatsopt / openmdao_extensions
  OpenMDAO solvers and drivers to handle specific methods.
  ☆11Updated 2 weeks ago
• mdolab / CMPLXFOIL
  ☆37Updated 3 weeks ago
• supaero-aircraft-design / FAST-GA
  FAST-(OAD)-GA is a framework for performing rapid Overall Aircraft Design for General Aviation Aircraft
  ☆33Updated 3 weeks ago
• mdolab / MACH-Aero
  MACH: MDO of Aircraft Configurations with High fidelity
  ☆125Updated last week
• OpenMDAO / dymos
  Open Source Optimization of Dynamic Multidisciplinary Systems
  ☆243Updated this week
• mdobook / resources
  Supplementary resources for the textbook Engineering Design Optimization by Joaquim R. R. A. Martins and Andrew Ning
  ☆112Updated 3 years ago
• cfsengineering / CEASIOMpy
  CEASIOMpy is a Python conceptual aircraft design environment
  ☆95Updated this week
• OpenMDAO / RevHack2020
  OpenMDAO 2020 Reverse Hackathon
  ☆14Updated 7 months ago
• smdogroup / tacs
  Finite-element library for analysis and adjoint-based gradient evaluation
  ☆117Updated last week
• mdolab / AerostructuralOptBenchmark
  ☆12Updated 3 months ago
• aqreed / PyVLM
  Vortex Lattice Method library written in Python
  ☆41Updated 5 years ago
• pedrosecchi67 / LovelacePM
  Open source, python-interpretable vortex panel method design to optimize aircraft configuration studies
  ☆38Updated 4 years ago
• DARcorporation / xrotor-python
  Stripped down version of XROTOR as compiled python module
  ☆21Updated 2 years ago
• WISDEM / CCBlade
  A blade element momentum method for analyzing wind turbine aerodynamic performance that is robust (guaranteed convergence), fast (superli…
  ☆48Updated last year
• VahanaOpenSource / vtol_sizing
  conceptual design of vtol platforms
  ☆14Updated 6 years ago
• whatsopt / WhatsOpt
  Web application for multidisciplinary design analysis and optimization
  ☆31Updated 2 weeks ago
• kegiljarhus / pyBEMT
  Implementation of the Blade Element Momentum Theory for turbines and propellers in Python
  ☆65Updated 2 years ago
• cotri / BEMT
  Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering
  ☆43Updated 2 years ago
• airinnova / pytornado
  An implementation of the vortex-lattice method (VLM)
  ☆31Updated last year
• SaTa999 / pyPanair
  A pre/post processor for PANAIR
  ☆15Updated 4 years ago