Alternatives and similar repositories for CPACS:

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

• cfsengineering / CEASIOMpy
  CEASIOMpy is a Python conceptual aircraft design environment
  ☆83Updated 2 months ago
• DLR-SC / tixi
  A simple XML interface library
  ☆36Updated 8 months ago
• OpenMDAO / Aviary
  NASA's aircraft analysis, design, and optimization tool
  ☆153Updated this week
• fast-aircraft-design / FAST-OAD
  FAST-OAD: An open source framework for rapid Overall Aircraft Design
  ☆58Updated this week
• mdolab / OpenAeroStruct
  OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.
  ☆199Updated this week
• OpenMDAO / pyCycle
  Thermodynamic cycle modeling library, built on top of OpenMDAO
  ☆88Updated 4 months ago
• DARcorporation / xfoil-python
  Stripped down version of XFOIL as compiled python module
  ☆90Updated 3 years ago
• DLR-SC / tigl
  The TiGL Geometry Library to process aircraft geometries in pre-design.
  ☆242Updated this week
• mdolab / openconcept
  OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures
  ☆37Updated 6 months ago
• OpenVOGEL / Tucan
  Tucan remains among the simplest and most user friendly programs for aerodynamics based on vortex lattice methods. This project is unique…
  ☆73Updated 8 months ago
• whatsopt / WhatsOpt
  Web application for multidisciplinary design analysis and optimization
  ☆31Updated 3 weeks ago
• mdolab / pyXDSM
  A python library for generating PDF XDSM diagrams.
  ☆59Updated last year
• OpenMDAO / mphys
  Multiphysics with OpenMDAO
  ☆78Updated this week
• OpenMDAO / POEMs
  Proposals for OpenMDAO Enhancements
  ☆14Updated 5 months ago
• DLR-AE / PanelAero
  An Implementation of the Vortex Lattice (VLM) and the Doublet Lattice Method (DLM) for aeroelasticity.
  ☆21Updated 4 months ago
• vtpasquale / NASTRAN_CoFE
  A finite element code for structural analysis. Written in MATLAB. Uses Nastran input format.
  ☆57Updated last year
• mdolab / MACH-Aero
  MACH: MDO of Aircraft Configurations with High fidelity
  ☆117Updated last month
• OpenMDAO / RevHack2020
  OpenMDAO 2020 Reverse Hackathon
  ☆14Updated 4 months ago
• 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…
  ☆15Updated last week
• aqreed / PyVLM
  Vortex Lattice Method library written in Python
  ☆41Updated 5 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…
  ☆69Updated 3 years ago
• VahanaOpenSource / vtol_sizing
  conceptual design of vtol platforms
  ☆13Updated 5 years ago
• smdogroup / tacs
  Finite-element library for analysis and adjoint-based gradient evaluation
  ☆114Updated this week
• nasa / pyturbo-aero
  Turbomachinery Blade and Flow path design tool
  ☆34Updated 3 weeks ago
• pedrosecchi67 / LovelacePM
  Open source, python-interpretable vortex panel method design to optimize aircraft configuration studies
  ☆38Updated 4 years ago
• airinnova / pytornado
  An implementation of the vortex-lattice method (VLM)
  ☆27Updated last year
• supaero-aircraft-design / FAST-GA
  FAST-(OAD)-GA is a framework for performing rapid Overall Aircraft Design for General Aviation Aircraft
  ☆33Updated this week
• kegiljarhus / pyBEMT
  Implementation of the Blade Element Momentum Theory for turbines and propellers in Python
  ☆60Updated 2 years ago
• ImperialCollegeLondon / sharpy
  Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code
  ☆130Updated last month
• pointwise / AircraftMesher
  A Glyph script demonstrating how to automate viscous meshing for aircraft geometry.
  ☆22Updated 3 years ago