An Open-Source Framework for Electric Propulsion System Analysis and Optimization in UAV Design
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Updated
Sep 8, 2026 - Python
An Open-Source Framework for Electric Propulsion System Analysis and Optimization in UAV Design
Minimal F# wrappers for Confluent.Kafka+librdkafka.redist 1.x
Imperial College London Aeronautical Engineering (MEng 4YFT) Study Materials
Example app and service templates `dotnet new -i Equinox.Templates; dotnet new eqx*/pro*` https://github.com/jet/equinox https://github.com/jet/FsCodec
Open source, 0-dimensional, object-oriented airbreathing engine modelling package for preliminary analysis and design of airbreathing engines, divulgation and educational purposes.
Notes and material for ME 461/561 Gas Dynamics course
The ultimate electric propulsion modeling and optimization module.
Notes and material for Rocket Propulsion course
An object-oriented Python 3 GUI and API for single- and multi-element parametric airfoil design, analysis, and optimization
A comprehensive solution for designing and optimizing student-built liquid rocket engines.
A MATLAB GUI for estimating some properties of turbines, the code is mainly based on Mattingly's "Elements of Propulsion". This repository is made for educational purposes, it does solve the problems in the book so it would be a useful resource for students. See the interface screenshots or just run the code, it's pre-loaded with examples!
Hybrid Rocket Propulsion Model [Python]
6-DoF hypersonic vehicle flight dynamics model coupled with a one-dimensional scramjet thermodynamic engine, including integrated guidance, navigation, and control.
CFD simulation of an aeroacoustic oscillating resonator using the Lattice Boltzmann Method (D2Q9). Visualise thrust generation via dynamic boundary layer and asymmetric fluid resistance accumulation.
A comprehensive repository for designing, simulating, and analyzing thermal protection systems and heat shielding for spacecraft and rockets.
🚀 Professional rocket engine simulation & 6-DOF flight analysis platform. NASA CEA validated thermochemistry, real-time performance calculations, Monte Carlo dispersion analysis.
🚀 Rocket calculations in Python using Cantera
An OpenFOAM-based software tool for Internal Ballistic simulations of solid rocket motors.
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