Alternatives and similar repositories for pypropep

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

• OpenVOGEL / Tucan
  Tucan remains among the simplest and most user friendly programs for aerodynamics based on vortex lattice methods. This project is unique…
  ☆78Updated last year
• mvernacc / proptools
  Rocket propulsion design calculation tools
  ☆51Updated 2 years ago
• Davide-sd / pygasflow
  Python functions for Quasi-1D Gasdynamics
  ☆26Updated 9 months ago
• mdolab / OpenAeroStruct
  OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.
  ☆235Updated this week
• DARcorporation / xfoil-python
  Stripped down version of XFOIL as compiled python module
  ☆104Updated 4 years ago
• sonofeft / RocketCEA
  RocketCEA Wraps The NASA Fortran CEA Code
  ☆119Updated 5 months ago
• cfsengineering / CEASIOMpy
  CEASIOMpy is a Python conceptual aircraft design environment
  ☆121Updated this week
• nasa / Three-Dimensional-Nozzle-Design-Code
  ☆54Updated 5 years ago
• OpenMDAO / pyCycle
  Thermodynamic cycle modeling library, built on top of OpenMDAO
  ☆131Updated 2 months ago
• PurdueH2Lab / MatlabCEA
  A Matlab interface for NASA CEA
  ☆33Updated 5 years ago
• suavecode / Tutorials
  This is where the tutorial scripts live
  ☆24Updated 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…
  ☆74Updated 4 years ago
• ravi4ram / Bell-Nozzle
  This script plots Bell Nozzle (Thrust Optimised Parabolic (TOP) nozzle) for the given area-ratio and throat radius.
  ☆28Updated 9 months ago
• mvernacc / aerospike-nozzle-design-gui
  Graphical software for designing aerospike rocket nozzles
  ☆33Updated 5 years ago
• AeroPython / scikit-aero
  Aeronautical engineering calculations in Python.
  ☆128Updated last year
• OpenMDAO / Aviary
  NASA's aircraft analysis, design, and optimization tool
  ☆225Updated last week
• chiefenne / PyAero
  PyAero is an open-source airfoil contour analysis and CFD meshing tool.
  ☆214Updated last month
• sonofeft / RocketIsp
  Rocketisp Calculates Delivered Specific Impulse (Isp) For Liquid Rocket Thrust Chambers.
  ☆15Updated 7 months ago
• cuspaceflight / bamboo
  Cooling system modelling for liquid rocket engines.
  ☆27Updated last year
• sobester / ADRpy
  Aircraft Design Recipes in Python
  ☆122Updated last year
• AeroDME / NASTRAN-95
  All updates to this code are to get NASTRAN-95 running in a GNU environment. It even runs on a Raspberry Pi! Some recent changes to the …
  ☆36Updated 5 years ago
• nasa / pyturbo-aero
  Turbomachinery Blade and Flow path design tool
  ☆60Updated 2 weeks ago
• psas / pintle-injector
  Pintle injector design for all PSAS liquid propellant engines
  ☆16Updated 4 years ago
• jvencels / EOF-Library
  Efficient two-way coupling between Elmer FEM and OpenFOAM
  ☆77Updated last year
• nasa / turbo-design
  Radial Equilibrium Code to design Turbomachinery
  ☆37Updated last week
• specifics / aero-structures
  Resources for analyzing aircraft structures for aerospace engineers
  ☆42Updated 5 years ago
• partmor / ezaero
  ezaero - Easy aerodynamics in Python
  ☆33Updated 4 years ago
• hystrath / hyStrath
  Hypersonic / Rarefied gas dynamics code developments (GPL-3.0)
  ☆248Updated 2 years ago
• mdolab / openconcept
  OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures
  ☆50Updated last week
• ImperialCollegeLondon / sharpy
  Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code
  ☆161Updated last month