Progdrasil / CEAMatlabAPI
Integration of NASA CEA into MATLAB for project at École Polytechnique de Montréal
☆12Updated 5 years ago
Alternatives and similar repositories for CEAMatlabAPI:
Users that are interested in CEAMatlabAPI are comparing it to the libraries listed below
- RocketProps calculates the various liquid propellant properties required to analyse a liquid propellant thrust chamber.☆18Updated last month
- Centrifugal Pump Design Tool Script☆12Updated 2 years ago
- Materials for the 2019 National Combustion Meeting Cantera Workshop☆12Updated 6 years ago
- Non-AXisymmetric aerodynamic design system for turbomachinery☆17Updated 4 years ago
- Rocket engine simulation for university projects☆10Updated 5 years ago
- A code based on the Method of Characteristics to solve the supersonic flow inside a nozzle☆11Updated 5 years ago
- This script plots Bell Nozzle (Thrust Optimised Parabolic (TOP) nozzle) for the given area-ratio and throat radius.☆22Updated 3 months ago
- A Matlab interface for NASA CEA☆31Updated 5 years ago
- ☆49Updated 4 years ago
- A MATLAB tool for the mean-line design optimization of axial turbines☆32Updated 4 years ago
- Multall-open is a turbomachinery design system based on the 3D, multistage, Navier-Stokes solver Multall. It can be used to design axial…☆23Updated 5 years ago
- Examples for RPA - Tool for Rocket Propulsion Analysis☆16Updated 8 years ago
- A Matlab tool for designing and analysing Regeneratively Cooled Liquid Rocket Engines☆10Updated 7 years ago
- T-Blade3 VERSION 1.2: T-Blade3 is a general parametric 3D blade geometry builder. The tool can create a variety of 3D blade geometries ba…☆50Updated 2 years ago
- Vortex Lattice for Aeroelasticity☆12Updated 7 years ago
- ☆37Updated last month
- Notes and material for ME 461/561 Gas Dynamics course☆27Updated 3 years ago
- ☆49Updated 7 years ago
- Turbomachinery Blade and Flow path design tool☆43Updated last week
- A python based blade parametrization tool☆53Updated 8 months ago
- ☆23Updated 7 years ago
- Supersonic Impulse Turbine Blade Design☆11Updated 6 years ago
- ☆24Updated 12 years ago
- Kinetic Approach to Physical Processes in Atmospheres☆22Updated 10 months ago
- Rocketisp Calculates Delivered Specific Impulse (Isp) For Liquid Rocket Thrust Chambers.☆12Updated last month
- Computational Fluid Dynamics, Waves, Reactions, Plasmas☆46Updated this week
- A pre/post processor for PANAIR☆15Updated 4 years ago
- Generate 4 and 5 digit NACA airfoil sections☆38Updated 6 months ago
- The Thermal Systems Analysis Toolbox (TSAT) is a MATLAB/Simulink based tool for modeling and analysis of dynamic thermal systems involvin…☆33Updated 6 years ago
- Unsteady Vortex Lattice Method for Aeroelasticity in C++☆23Updated last year