lpre / RPA-ExamplesLinks
Examples for RPA - Tool for Rocket Propulsion Analysis
☆17Updated 8 years ago
Alternatives and similar repositories for RPA-Examples
Users that are interested in RPA-Examples are comparing it to the libraries listed below
Sorting:
- ☆54Updated 4 years ago
- Integration of NASA CEA into MATLAB for project at École Polytechnique de Montréal☆12Updated 5 years ago
- Tucan remains among the simplest and most user friendly programs for aerodynamics based on vortex lattice methods. This project is unique…☆76Updated last year
- RocketCEA Wraps The NASA Fortran CEA Code☆114Updated 2 months ago
- RocketProps calculates the various liquid propellant properties required to analyse a liquid propellant thrust chamber.☆21Updated 4 months ago
- A Matlab interface for NASA CEA☆32Updated 5 years ago
- Graphical software for designing aerospike rocket nozzles☆33Updated 4 years ago
- This script plots Bell Nozzle (Thrust Optimised Parabolic (TOP) nozzle) for the given area-ratio and throat radius.☆24Updated 6 months ago
- Non-AXisymmetric aerodynamic design system for turbomachinery☆18Updated 4 years ago
- Turbomachinery Blade and Flow path design tool☆52Updated last week
- Rocket propulsion design calculation tools☆51Updated 2 years ago
- ☆25Updated 12 years ago
- Python Tools to Practically Model and Solve the Problem of High Speed Rotor Balancing.☆25Updated last year
- Rocket engine simulation for university projects☆10Updated 5 years ago
- The Thermal Systems Analysis Toolbox (TSAT) is a MATLAB/Simulink based tool for modeling and analysis of dynamic thermal systems involvin…☆35Updated 6 years ago
- Design of turbomachine blade profile☆34Updated 11 months ago
- Multi-disciplinary optimization for Launch Vehicle 4 and it's LOX/IPA liquid fuel engine.☆24Updated 2 years ago
- A code based on the Method of Characteristics to solve the supersonic flow inside a nozzle☆11Updated 5 years ago
- CPACS - Common Parametric Aircraft Configuration Schema☆89Updated 2 months ago
- OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.☆223Updated 3 weeks ago
- Thermodynamic cycle modeling library, built on top of OpenMDAO☆118Updated 3 weeks ago
- Cooling system modelling for liquid rocket engines.☆26Updated 9 months ago
- Gas models, combustion and gas turbine solver.☆75Updated 2 years ago
- ☆39Updated 3 months ago
- Rocketisp Calculates Delivered Specific Impulse (Isp) For Liquid Rocket Thrust Chambers.☆14Updated 4 months ago
- ☆23Updated 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…☆72Updated 4 years ago
- PyAero is an open-source airfoil contour analysis and CFD meshing tool.☆205Updated 6 months ago
- A MATLAB tool for the mean-line design optimization of axial turbines☆33Updated 4 years ago
- This is a graphical user interface for Mark Drela's Athena Vortex Lattice (AVL) and XFoil☆12Updated 4 months ago