Alternatives and similar repositories for openconcept

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

• fast-aircraft-design / FAST-OAD
  FAST-OAD: An open source framework for rapid Overall Aircraft Design
  ☆77Updated last month
• cfsengineering / CEASIOMpy
  CEASIOMpy is a Python conceptual aircraft design environment
  ☆136Updated this week
• mdolab / OpenAeroStruct
  OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.
  ☆243Updated 3 months ago
• ImperialCollegeLondon / sharpy
  Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code
  ☆171Updated 2 weeks ago
• OpenMDAO / Aviary
  NASA's aircraft analysis, design, and optimization tool
  ☆245Updated this 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
• mdolab / pyXDSM
  A python library for generating PDF XDSM diagrams.
  ☆71Updated 4 months ago
• byuflowlab / CCBlade.jl
  Blade Element Momentum Method for Propellers and Turbines
  ☆76Updated last month
• OpenMDAO / pyCycle
  Thermodynamic cycle modeling library, built on top of OpenMDAO
  ☆150Updated 3 months ago
• OpenMDAO / mphys
  Multiphysics with OpenMDAO
  ☆116Updated last month
• byuflowlab / FLOWUnsteady
  An interactional aerodynamics and acoustics solver for multirotor aircraft and wind energy
  ☆350Updated 4 months ago
• cotri / BEMT
  Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering
  ☆55Updated 3 years ago
• DARcorporation / xfoil-python
  Stripped down version of XFOIL as compiled python module
  ☆108Updated 4 years ago
• sobester / airgeobookcode_m
  Matlab code to accompany "Aircraft Aerodynamic Design: Geometry and Optimization" by Sobester and Forrester (2015)
  ☆20Updated 6 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…
  ☆49Updated 8 years ago
• kegiljarhus / pyBEMT
  Implementation of the Blade Element Momentum Theory for turbines and propellers in Python
  ☆80Updated 3 years ago
• DLR-AE / PanelAero
  An Implementation of the Vortex Lattice (VLM) and the Doublet Lattice Method (DLM) for aeroelasticity.
  ☆42Updated last month
• ideas-um / FAST
  Future Aircraft Sizing Tool
  ☆109Updated this week
• VahanaOpenSource / vtol_sizing
  conceptual design of vtol platforms
  ☆18Updated 6 years ago
• mdolab / MACH-Aero
  MACH: MDO of Aircraft Configurations with High fidelity
  ☆148Updated 2 months ago
• aqreed / PyVLM
  Vortex Lattice Method library written in Python
  ☆44Updated 6 years 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…
  ☆76Updated 4 years ago
• airinnova / pytornado
  An implementation of the vortex-lattice method (VLM)
  ☆38Updated 2 years ago
• mdolab / CMPLXFOIL
  ☆39Updated this week
• usuaero / MachLine
  A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.
  ☆47Updated 10 months ago
• supaero-aircraft-design / FAST-GA
  FAST-(OAD)-GA is a framework for performing rapid Overall Aircraft Design for General Aviation Aircraft
  ☆37Updated 2 weeks ago
• DLR-SL / CPACS
  CPACS - Common Parametric Aircraft Configuration Schema
  ☆97Updated last week
• raalf / BEMT
  Blade element momentum theory approach to calculate blade forces at varying inflow angles
  ☆11Updated 6 years ago
• SaTa999 / pyPanair
  A pre/post processor for PANAIR
  ☆20Updated 5 years ago
• seyk86 / dAEDalusNXT
  Aeroelastic Aircraft Design and Simulation Tool
  ☆29Updated 7 years ago