Alternatives and similar repositories for Bell-Nozzle

Users that are interested in Bell-Nozzle are comparing it to the libraries listed below

• nasa / Three-Dimensional-Nozzle-Design-Code
  ☆54Updated 5 years ago
• Progdrasil / CEAMatlabAPI
  Integration of NASA CEA into MATLAB for project at École Polytechnique de Montréal
  ☆13Updated 6 years ago
• PurdueH2Lab / MatlabCEA
  A Matlab interface for NASA CEA
  ☆34Updated 5 years ago
• sonofeft / RocketProps
  RocketProps calculates the various liquid propellant properties required to analyse a liquid propellant thrust chamber.
  ☆23Updated 8 months ago
• sonofeft / RocketCEA
  RocketCEA Wraps The NASA Fortran CEA Code
  ☆120Updated 6 months ago
• nasa / pyturbo-aero
  Turbomachinery Blade and Flow path design tool
  ☆64Updated last month
• mvernacc / proptools
  Rocket propulsion design calculation tools
  ☆52Updated 3 years ago
• mdolab / OpenAeroStruct
  OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.
  ☆236Updated last month
• aero29 / NAX
  Non-AXisymmetric aerodynamic design system for turbomachinery
  ☆18Updated 5 years ago
• hystrath / hyStrath
  Hypersonic / Rarefied gas dynamics code developments (GPL-3.0)
  ☆251Updated 2 years ago
• turbo-sim / AxialOpt
  A MATLAB tool for the mean-line design optimization of axial turbines
  ☆35Updated 4 years 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
• 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…
  ☆22Updated 7 years ago
• cfsengineering / CEASIOMpy
  CEASIOMpy is a Python conceptual aircraft design environment
  ☆128Updated this week
• OpenMDAO / pyCycle
  Thermodynamic cycle modeling library, built on top of OpenMDAO
  ☆137Updated 3 weeks ago
• nasa / cfdtools
  ☆135Updated 2 years ago
• xavierdechamps / Nozzle_MOC_supersonic
  A code based on the Method of Characteristics to solve the supersonic flow inside a nozzle
  ☆10Updated 6 years ago
• OpenMDAO / mphys
  Multiphysics with OpenMDAO
  ☆112Updated 2 months ago
• nasa / turbo-design
  Radial Equilibrium Code to design Turbomachinery
  ☆40Updated last month
• SaTa999 / pyPanair
  A pre/post processor for PANAIR
  ☆18Updated 4 years ago
• mdolab / MACH-Aero
  MACH: MDO of Aircraft Configurations with High fidelity
  ☆145Updated last week
• sobester / airgeobookcode_m
  Matlab code to accompany "Aircraft Aerodynamic Design: Geometry and Optimization" by Sobester and Forrester (2015)
  ☆19Updated 6 years ago
• OpenVOGEL / Tucan
  Tucan remains among the simplest and most user friendly programs for aerodynamics based on vortex lattice methods. This project is unique…
  ☆79Updated last year
• nasa / T-MATS
  An open source thermodynamic modeling package completed on behalf of NASA. The Toolbox for the Modeling and Analysis of Thermodynamic Sys…
  ☆294Updated 9 months ago
• precise-simulation / cfdtool
  CFDTool - An easy to use OpenFOAM / SU2 / CFD simulation toolbox
  ☆97Updated 3 months ago
• kyleniemeyer / gas-dynamics-notes
  Notes and material for ME 461/561 Gas Dynamics course
  ☆27Updated 3 years ago
• 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 …
  ☆37Updated 5 years ago
• kegiljarhus / pyBEMT
  Implementation of the Blade Element Momentum Theory for turbines and propellers in Python
  ☆71Updated 3 years ago
• Interfluo / OpenFOAM-Cases-Interfluo
  OpenFOAM cases from my YouTube channel
  ☆106Updated last year
• DLR-AE / PanelAero
  An Implementation of the Vortex Lattice (VLM) and the Doublet Lattice Method (DLM) for aeroelasticity.
  ☆38Updated 2 months ago