sonofeft / RocketCEALinks
RocketCEA Wraps The NASA Fortran CEA Code
☆111Updated last month
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☆32Updated 5 years ago
- ☆51Updated 4 years ago
- A Python wrapper to use the Chemical Equilibrium with Applications Fortran code☆14Updated 8 years ago
- Turbomachinery Blade and Flow path design tool☆47Updated last week
- Hypersonic / Rarefied gas dynamics code developments (GPL-3.0)☆242Updated last year
- This script plots Bell Nozzle (Thrust Optimised Parabolic (TOP) nozzle) for the given area-ratio and throat radius.☆23Updated 5 months ago
- ☆122Updated 2 years ago
- RocketProps calculates the various liquid propellant properties required to analyse a liquid propellant thrust chamber.☆19Updated 3 months ago
- Rocket propulsion design calculation tools☆50Updated 2 years ago
- CEASIOMpy is a Python conceptual aircraft design environment☆107Updated this week
- Python functions for Quasi-1D Gasdynamics☆23Updated 5 months ago
- The MUlticomponent Thermodynamic And Transport library for IONized gases in C++☆117Updated 11 months ago
- Multiphysics with OpenMDAO☆105Updated last month
- Porous Material Analysis Toolbox☆20Updated last year
- Cooling system modelling for liquid rocket engines.☆23Updated 8 months ago
- Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code☆157Updated this week
- PICLas is a parallel, three-dimensional PIC-DSMC solver developed cooperatively by the Institute of Space Systems, Institute of Aerodynam…☆85Updated 5 months ago
- Stripped down version of XFOIL as compiled python module☆99Updated 3 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…☆71Updated 4 years ago
- OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.☆216Updated last month
- Thermodynamic cycle modeling library, built on top of OpenMDAO☆108Updated last week
- OpenFOAM tutorial cases with comprehensive instructions.☆86Updated 6 years ago
- Rocketisp Calculates Delivered Specific Impulse (Isp) For Liquid Rocket Thrust Chambers.☆14Updated 3 months ago
- Gas models, combustion and gas turbine solver.☆74Updated 2 years ago
- ☆37Updated 2 months ago
- NASA's aircraft analysis, design, and optimization tool☆191Updated this week
- OpenFOAM cases from my YouTube channel☆103Updated 11 months ago
- An axial compressor design code compatible with applications using Supercritical Carbon Dioxide (S-CO2). Written in Python for portabilit…☆15Updated last year
- Documentation on our model development, currently only notes on the use of OpenFOAM☆133Updated 2 weeks ago
- OpenFOAM Foundation repository for OpenFOAM version 7☆100Updated 4 years ago