Alternatives and similar repositories for pyCycle

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

• OpenMDAO / mphys
  Multiphysics with OpenMDAO
  ☆113Updated 2 weeks ago
• DARcorporation / xfoil-python
  Stripped down version of XFOIL as compiled python module
  ☆105Updated 4 years ago
• mdolab / OpenAeroStruct
  OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.
  ☆239Updated 2 months ago
• fast-aircraft-design / FAST-OAD
  FAST-OAD: An open source framework for rapid Overall Aircraft Design
  ☆76Updated 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…
  ☆74Updated 4 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…
  ☆48Updated 8 years ago
• mdolab / MACH-Aero
  MACH: MDO of Aircraft Configurations with High fidelity
  ☆145Updated last month
• mdolab / pyXDSM
  A python library for generating PDF XDSM diagrams.
  ☆71Updated 3 months ago
• mdolab / CMPLXFOIL
  ☆38Updated this week
• ImperialCollegeLondon / sharpy
  Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code
  ☆169Updated this week
• mdolab / adflow
  ADflow is a finite volume RANS solver tailored for gradient-based aerodynamic design optimization.
  ☆285Updated 3 weeks ago
• whatsopt / WhatsOpt
  Web application for multidisciplinary design analysis and optimization
  ☆32Updated last week
• NAnand-TUD / parablade
  A python based blade parametrization tool
  ☆65Updated last year
• mdolab / pygeo
  pyGeo provides geometric design variables and constraints suitable for gradient-based optimization.
  ☆192Updated last week
• cfsengineering / CEASIOMpy
  CEASIOMpy is a Python conceptual aircraft design environment
  ☆133Updated last week
• mdolab / openconcept
  OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures
  ☆52Updated last month
• whatsopt / openmdao_extensions
  OpenMDAO solvers and drivers to handle specific methods.
  ☆12Updated last month
• mdolab / dafoam
  DAFoam: Discrete Adjoint with OpenFOAM for High-fidelity Multidisciplinary Design Optimization
  ☆298Updated this week
• airinnova / pytornado
  An implementation of the vortex-lattice method (VLM)
  ☆38Updated 2 years ago
• MRod5 / pyturb
  Gas models, combustion and gas turbine solver.
  ☆77Updated 2 years ago
• chiefenne / PyAero
  PyAero is an open-source airfoil contour analysis and CFD meshing tool.
  ☆223Updated 3 months ago
• byuflowlab / CCBlade.jl
  Blade Element Momentum Method for Propellers and Turbines
  ☆72Updated last week
• DLR-AE / LoadsKernel
  The Loads Kernel Software allows for the calculation of quasi-steady and dynamic maneuver loads, unsteady gust loads in the time and freq…
  ☆27Updated last week
• kegiljarhus / pyBEMT
  Implementation of the Blade Element Momentum Theory for turbines and propellers in Python
  ☆77Updated 3 years ago
• marilib / MARILib
  Multidisciplinary Airplane Research Integrated Library
  ☆11Updated 5 years ago
• smdogroup / tacs
  Finite-element library for analysis and adjoint-based gradient evaluation
  ☆133Updated last month
• DLR-SL / CPACS
  CPACS - Common Parametric Aircraft Configuration Schema
  ☆97Updated last month
• usuaero / MachLine
  A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.
  ☆45Updated 9 months ago
• partmor / ezaero
  ezaero - Easy aerodynamics in Python
  ☆33Updated 5 years ago
• snl-dakota / dakota
  The core Dakota project
  ☆130Updated last week