Alternatives and similar repositories for material-properties-interchange

Users that are interested in material-properties-interchange are comparing it to the libraries listed below

• OpenMDAO / EngSketchPad
  ☆27Updated 13 years ago
• OpenMDAO / pyCycle
  Thermodynamic cycle modeling library, built on top of OpenMDAO
  ☆135Updated 2 weeks ago
• DLR-SL / CPACS
  CPACS - Common Parametric Aircraft Configuration Schema
  ☆96Updated 2 weeks ago
• nasa / TSAT
  The Thermal Systems Analysis Toolbox (TSAT) is a MATLAB/Simulink based tool for modeling and analysis of dynamic thermal systems involvin…
  ☆37Updated 7 years ago
• sonofeft / RocketProps
  RocketProps calculates the various liquid propellant properties required to analyse a liquid propellant thrust chamber.
  ☆23Updated 8 months ago
• nasa / Three-Dimensional-Nozzle-Design-Code
  ☆54Updated 5 years ago
• CoolProp / GUI
  A python-based graphical user interface for CoolProp
  ☆21Updated 3 years ago
• ina111 / CentrifugalPump_DesignTool
  Centrifugal Pump Design Tool Script
  ☆13Updated 2 years ago
• mdolab / OpenAeroStruct
  OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.
  ☆236Updated 3 weeks ago
• OpenMDAO / mphys
  Multiphysics with OpenMDAO
  ☆113Updated last month
• vtpasquale / NASTRAN_CoFE
  A finite element code for structural analysis. Written in MATLAB. Uses Nastran input format.
  ☆60Updated last week
• nasa / pyturbo-aero
  Turbomachinery Blade and Flow path design tool
  ☆62Updated last month
• VahanaOpenSource / vtol_sizing
  conceptual design of vtol platforms
  ☆17Updated 6 years ago
• MYSTRANsolver / MYSTRAN
  MYSTRAN is a general purpose finite element analysis solver
  ☆89Updated 2 weeks ago
• mdolab / CMPLXFOIL
  ☆39Updated last month
• cfsengineering / CEASIOMpy
  CEASIOMpy is a Python conceptual aircraft design environment
  ☆122Updated 2 weeks 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…
  ☆26Updated 2 months ago
• DARcorporation / xrotor-python
  Stripped down version of XROTOR as compiled python module
  ☆23Updated 2 years ago
• sonofeft / RocketIsp
  Rocketisp Calculates Delivered Specific Impulse (Isp) For Liquid Rocket Thrust Chambers.
  ☆15Updated 8 months ago
• turbo-sim / AxialOpt
  A MATLAB tool for the mean-line design optimization of axial turbines
  ☆35Updated 4 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…
  ☆74Updated 4 years ago
• qingfengxia / Cfd
  Computional Fluid Dynamics (CFD) for FreeCAD based on OpenFOAM and Fenics solver
  ☆203Updated 3 years ago
• GeneralElectric / CalculiX
  CalculiX is an OSS package designed to solve field problems. The method used is the finite element method. This package is a native Micro…
  ☆124Updated 9 years ago
• chiefenne / PyAero
  PyAero is an open-source airfoil contour analysis and CFD meshing tool.
  ☆218Updated last month
• boschresearch / pylife
  a general library for fatigue and reliability
  ☆168Updated last week
• vsdsantos / nastran-aeroelasticity
  Some usefull routines for aeroelastic analysis with NASTRAN.
  ☆21Updated 3 years ago
• Progdrasil / CEAMatlabAPI
  Integration of NASA CEA into MATLAB for project at École Polytechnique de Montréal
  ☆13Updated 6 years ago
• DARcorporation / xfoil-python
  Stripped down version of XFOIL as compiled python module
  ☆104Updated 4 years ago
• DLR-AE / PanelAero
  An Implementation of the Vortex Lattice (VLM) and the Doublet Lattice Method (DLM) for aeroelasticity.
  ☆38Updated 2 months ago
• NAnand-TUD / parablade
  A python based blade parametrization tool
  ☆65Updated last year