PurdueH2Lab / MatlabCEA
A Matlab interface for NASA CEA
☆31Updated 5 years ago
Alternatives and similar repositories for MatlabCEA:
Users that are interested in MatlabCEA are comparing it to the libraries listed below
- ☆49Updated 4 years ago
- Turbomachinery Blade and Flow path design tool☆38Updated this week
- RocketCEA Wraps The NASA Fortran CEA Code☆101Updated 3 weeks ago
- ☆23Updated 7 years ago
- The Thermal Systems Analysis Toolbox (TSAT) is a MATLAB/Simulink based tool for modeling and analysis of dynamic thermal systems involvin…☆32Updated 6 years ago
- CEASIOMpy is a Python conceptual aircraft design environment☆88Updated this week
- ☆20Updated 7 years ago
- Free and open-source solid rocket motor design and internal ballistics simulation☆15Updated 6 years ago
- RocketProps calculates the various liquid propellant properties required to analyse a liquid propellant thrust chamber.☆18Updated 3 weeks ago
- Integration of NASA CEA into MATLAB for project at École Polytechnique de Montréal☆12Updated 5 years ago
- Stripped down version of XFOIL as compiled python module☆94Updated 3 years ago
- This script plots Bell Nozzle (Thrust Optimised Parabolic (TOP) nozzle) for the given area-ratio and throat radius.☆22Updated 2 months ago
- ☆36Updated this week
- A Matlab tool for designing and analysing Regeneratively Cooled Liquid Rocket Engines☆9Updated 7 years ago
- Centrifugal Pump Design Tool Script☆12Updated last year
- Matlab code to accompany "Aircraft Aerodynamic Design: Geometry and Optimization" by Sobester and Forrester (2015)☆16Updated 6 years ago
- Cooling system modelling for liquid rocket engines.☆21Updated 5 months ago
- OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures☆40Updated 3 weeks ago
- Non-AXisymmetric aerodynamic design system for turbomachinery☆15Updated 4 years ago
- ☆48Updated 6 years ago
- Modified USAF Aircraft DATCOM☆20Updated 12 years ago
- Notes and material for ME 461/561 Gas Dynamics course☆27Updated 3 years ago
- Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering☆42Updated 2 years ago
- FAST-OAD: An open source framework for rapid Overall Aircraft Design☆60Updated this week
- 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 3 years ago
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python☆63Updated 2 years ago
- A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.☆39Updated 3 weeks ago
- A Python wrapper to use the Chemical Equilibrium with Applications Fortran code☆14Updated 8 years ago
- ☆113Updated 2 years ago
- Rocketisp Calculates Delivered Specific Impulse (Isp) For Liquid Rocket Thrust Chambers.☆12Updated 3 weeks ago