lpre / RPA-Examples
Examples for RPA - Tool for Rocket Propulsion Analysis
☆16Updated 8 years ago
Related projects ⓘ
Alternatives and complementary repositories for RPA-Examples
- Integration of NASA CEA into MATLAB for project at École Polytechnique de Montréal☆11Updated 5 years ago
- ☆44Updated 4 years ago
- Turbomachinery Blade and Flow path design tool☆30Updated this week
- RocketProps calculates the various liquid propellant properties required to analyse a liquid propellant thrust chamber.☆15Updated 5 months ago
- This script plots Bell Nozzle (Thrust Optimised Parabolic (TOP) nozzle) for the given area-ratio and throat radius.☆20Updated 3 months ago
- A Matlab interface for NASA CEA☆30Updated 4 years ago
- Multi-disciplinary optimization for Launch Vehicle 4 and it's LOX/IPA liquid fuel engine.☆24Updated last year
- Non-AXisymmetric aerodynamic design system for turbomachinery☆14Updated 4 years ago
- The Thermal Systems Analysis Toolbox (TSAT) is a MATLAB/Simulink based tool for modeling and analysis of dynamic thermal systems involvin…☆31Updated 6 years ago
- A code based on the Method of Characteristics to solve the supersonic flow inside a nozzle☆11Updated 5 years ago
- Tucan remains among the simplest and most user friendly programs for aerodynamics based on vortex lattice methods. This project is unique…☆72Updated 6 months ago
- Cooling system modelling for liquid rocket engines.☆17Updated last month
- Centrifugal Pump Design Tool Script☆12Updated last year
- A MATLAB tool for the mean-line design optimization of axial turbines☆27Updated 3 years ago
- ☆23Updated 12 years ago
- Rocket engine simulation for university projects☆9Updated 5 years ago
- A MATLAB GUI for estimating some properties of turbines, the code is mainly based on Mattingly's "Elements of Propulsion". This repositor…☆19Updated 6 years ago
- Vortex Lattice for Aeroelasticity☆10Updated 7 years ago
- A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.☆33Updated this week
- An Implementation of the Vortex Lattice (VLM) and the Doublet Lattice Method (DLM) for aeroelasticity.☆20Updated 2 months ago
- The Tip Clearance Modeling Library (TCML) was developed to model the dynamic variation of the high pressure turbine (HPT) tip clearance i…☆16Updated 6 years ago
- ☆45Updated 6 years ago
- All updates to this code are to get NASTRAN-95 running in a GNU environment. It even runs on a Raspberry Pi! Some recent changes to the …☆32Updated 4 years ago
- Free and open-source solid rocket motor design and internal ballistics simulation☆15Updated 6 years ago
- Unsteady Vortex Lattice Method for Aeroelasticity in C++☆23Updated last year
- Supersonic Impulse Turbine Blade Design☆11Updated 6 years ago
- conceptual design of vtol platforms☆13Updated 5 years ago
- Notes and material for ME 461/561 Gas Dynamics course☆22Updated 2 years ago
- Graphical software for designing aerospike rocket nozzles☆32Updated 4 years ago