sonofeft / RocketCEALinks
RocketCEA Wraps The NASA Fortran CEA Code
☆119Updated 6 months ago
Alternatives and similar repositories for RocketCEA
Users that are interested in RocketCEA are comparing it to the libraries listed below
Sorting:
- A Matlab interface for NASA CEA☆34Updated 5 years ago
- ☆54Updated 5 years ago
- RocketProps calculates the various liquid propellant properties required to analyse a liquid propellant thrust chamber.☆23Updated 8 months ago
- Rocketisp Calculates Delivered Specific Impulse (Isp) For Liquid Rocket Thrust Chambers.☆15Updated 8 months ago
- Rocket propulsion design calculation tools☆52Updated 3 years ago
- OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.☆236Updated 3 weeks ago
- Hypersonic / Rarefied gas dynamics code developments (GPL-3.0)☆251Updated 2 years ago
- Turbomachinery Blade and Flow path design tool☆64Updated last month
- ☆133Updated 2 years ago
- Thermodynamic cycle modeling library, built on top of OpenMDAO☆135Updated 2 weeks ago
- CEASIOMpy is a Python conceptual aircraft design environment☆122Updated this week
- Integration of NASA CEA into MATLAB for project at École Polytechnique de Montréal☆13Updated 6 years ago
- 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…☆73Updated 4 years ago
- 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's aircraft analysis, design, and optimization tool☆230Updated last week
- This script plots Bell Nozzle (Thrust Optimised Parabolic (TOP) nozzle) for the given area-ratio and throat radius.☆28Updated 10 months ago
- Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code☆164Updated last month
- 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
- ☆317Updated 3 years ago
- ☆38Updated last month
- Rocket engine simulation for university projects☆10Updated 6 years ago
- A Python wrapper to use the Chemical Equilibrium with Applications Fortran code☆16Updated 9 years ago
- OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures☆51Updated last week
- Gas models, combustion and gas turbine solver.☆76Updated 2 years ago
- Matlab code to accompany "Aircraft Aerodynamic Design: Geometry and Optimization" by Sobester and Forrester (2015)☆19Updated 6 years ago
- Stripped down version of XFOIL as compiled python module☆104Updated 4 years ago
- Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering☆52Updated 3 years ago
- A MATLAB tool for the mean-line design optimization of axial turbines☆35Updated 4 years ago
- Radial Equilibrium Code to design Turbomachinery☆39Updated 3 weeks ago
- OpenFOAM Foundation repository for OpenFOAM version 7☆102Updated 5 years ago