Alternatives and similar repositories for T-MATS

Users that are interested in T-MATS are comparing it to the libraries listed below

• cfsengineering / CEASIOMpy
  CEASIOMpy is a Python conceptual aircraft design environment
  ☆111Updated 3 weeks ago
• mdolab / OpenAeroStruct
  OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.
  ☆223Updated 2 weeks ago
• mdolab / openconcept
  OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures
  ☆45Updated this week
• nasa / TTECTrA
  An open source, semi-automated, control design tool for subsonic aircraft engine simulations written in the MATLAB/Simulink environment. …
  ☆64Updated 11 years ago
• MRod5 / pyturb
  Gas models, combustion and gas turbine solver.
  ☆75Updated 2 years ago
• OpenMDAO / Aviary
  NASA's aircraft analysis, design, and optimization tool
  ☆206Updated last week
• suavecode / SUAVE
  An Aircraft Design Toolbox
  ☆451Updated last year
• fast-aircraft-design / FAST-OAD
  FAST-OAD: An open source framework for rapid Overall Aircraft Design
  ☆68Updated this week
• nasa / AGTF30
  ☆34Updated last year
• DLR-SL / CPACS
  CPACS - Common Parametric Aircraft Configuration Schema
  ☆89Updated 2 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…
  ☆76Updated last year
• ImperialCollegeLondon / sharpy
  Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code
  ☆158Updated last month
• OpenMDAO / pyCycle
  Thermodynamic cycle modeling library, built on top of OpenMDAO
  ☆116Updated 2 weeks ago
• byuflowlab / FLOWUnsteady
  An interactional aerodynamics and acoustics solver for multirotor aircraft and wind energy
  ☆312Updated last month
• abdolrezat / TURBN-Turbine-Design
  A MATLAB GUI for estimating some properties of turbines, the code is mainly based on Mattingly's "Elements of Propulsion". This repositor…
  ☆23Updated 7 years ago
• nasa / pyturbo-aero
  Turbomachinery Blade and Flow path design tool
  ☆52Updated this week
• PurdueH2Lab / MatlabCEA
  A Matlab interface for NASA CEA
  ☆32Updated 5 years ago
• cotri / BEMT
  Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering
  ☆46Updated 3 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…
  ☆72Updated 4 years ago
• OpenMDAO / mphys
  Multiphysics with OpenMDAO
  ☆106Updated 2 months ago
• ideas-um / FAST
  Future Aircraft Sizing Tool
  ☆86Updated 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…
  ☆46Updated 7 years ago
• sobester / airgeobookcode_m
  Matlab code to accompany "Aircraft Aerodynamic Design: Geometry and Optimization" by Sobester and Forrester (2015)
  ☆17Updated 6 years ago
• suavecode / Tutorials
  This is where the tutorial scripts live
  ☆24Updated 3 years ago
• VahanaOpenSource / vtol_sizing
  conceptual design of vtol platforms
  ☆16Updated 6 years ago
• seyk86 / dAEDalusNXT
  Aeroelastic Aircraft Design and Simulation Tool
  ☆29Updated 7 years ago
• DARcorporation / airfoil-optimizer-web-ui
  Simple airfoil optimization problem using OpenMDAO
  ☆9Updated 2 years ago
• nasa / CFL3D
  ☆310Updated 2 years ago
• DARcorporation / xfoil-python
  Stripped down version of XFOIL as compiled python module
  ☆99Updated 4 years ago
• sobester / ADRpy
  Aircraft Design Recipes in Python
  ☆115Updated last year