Alternatives and similar repositories for WhatsOpt

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

• fast-aircraft-design / FAST-OAD
  FAST-OAD: An open source framework for rapid Overall Aircraft Design
  ☆73Updated this week
• OpenMDAO / mphys
  Multiphysics with OpenMDAO
  ☆112Updated last month
• OpenMDAO / pyCycle
  Thermodynamic cycle modeling library, built on top of OpenMDAO
  ☆131Updated 2 months ago
• mdolab / AerostructuralOptBenchmark
  ☆16Updated 2 months ago
• whatsopt / openmdao_extensions
  OpenMDAO solvers and drivers to handle specific methods.
  ☆12Updated last month
• marilib / MARILib
  Multidisciplinary Airplane Research Integrated Library
  ☆11Updated 5 years ago
• mdolab / OpenAeroStruct
  OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.
  ☆235Updated last week
• mdolab / pygeo
  pyGeo provides geometric design variables and constraints suitable for gradient-based optimization.
  ☆184Updated 2 weeks ago
• WISDEM / CCBlade
  A blade element momentum method for analyzing wind turbine aerodynamic performance that is robust (guaranteed convergence), fast (superli…
  ☆57Updated last month
• WISDEM / pBEAM
  A finite element method for beam-like structures.
  ☆12Updated 3 months ago
• 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…
  ☆73Updated 4 years ago
• LHEEA / meshmagick
  A command line tool and a python package to manipulate hydrodynamics meshes
  ☆51Updated 8 months ago
• mdolab / pyXDSM
  A python library for generating PDF XDSM diagrams.
  ☆70Updated last month
• whatsopt / XDSMjs
  XDSM generator written in javascript.
  ☆12Updated last year
• ANBA4 / anba4
  ☆14Updated last year
• mathLab / BladeX
  BladeX - Python Blade Morphing
  ☆78Updated 5 months ago
• DARcorporation / xfoil-python
  Stripped down version of XFOIL as compiled python module
  ☆104Updated 4 years ago
• DLR-SL / CPACS
  CPACS - Common Parametric Aircraft Configuration Schema
  ☆95Updated last month
• MRod5 / pyturb
  Gas models, combustion and gas turbine solver.
  ☆75Updated 2 years ago
• OpenMDAO / EngSketchPad
  ☆27Updated 12 years ago
• mdolab / CMPLXFOIL
  ☆39Updated last month
• pedrosecchi67 / LovelacePM
  Open source, python-interpretable vortex panel method design to optimize aircraft configuration studies
  ☆39Updated 5 years ago
• ImperialCollegeLondon / sharpy
  Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code
  ☆161Updated last month
• capytaine / capytaine
  Python BEM solver for linear potential flow, based on Nemoh.
  ☆183Updated this week
• NAnand-TUD / parablade
  A python based blade parametrization tool
  ☆64Updated last year
• cfsengineering / CEASIOMpy
  CEASIOMpy is a Python conceptual aircraft design environment
  ☆120Updated this week
• WISDEM / SONATA
  ☆13Updated last 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…
  ☆48Updated 8 years ago
• smdogroup / tacs
  Finite-element library for analysis and adjoint-based gradient evaluation
  ☆129Updated this week
• mdolab / MACH-Aero
  MACH: MDO of Aircraft Configurations with High fidelity
  ☆141Updated 3 weeks ago