Designing a ramjet engine using first principles of compressible flow. Components simulated include: inlet, diffuser, flameholder, combustor, converging and diverging nozzle.
-
Updated
Jun 21, 2024 - MATLAB
#
nozzle-design
Here are 6 public repositories matching this topic...
An implementation of the method of characteristics for supersonic nozzle design written in Python.
-
Updated
Aug 31, 2023 - Python
Conceptual design and analysis of a liquid-propellant rocket engine for orbital launch vehicles. Presents key specs (chamber pressure, nozzle expansion, thrust-to-weight), propellant/material selection (LOX/RP-1 & LOX/LH₂), cycle considerations, and computational workflows for engine sizing, sweeps and trade-off studies.
aerospace cea rocket-engine nozzle-design engine-design rocket-propulsion liquid-propellant orbital-launch-vehicle combustion-chamber thrust-to-weight lox-rp1 lox-lh2 propulsion-analysis spacecraft-engineering
-
Updated
Nov 6, 2025 - Python
TIC and TOP rocket nozzle contour synthesis
-
Updated
Apr 18, 2024 - Jupyter Notebook
A complete rewrite in Rust of the Hypersonic Nozzle Design Program (HNDP), originally implemented in C++.
-
Updated
Dec 10, 2025 - Rust
A GUI for Hypersonic Nozzle Design Program
-
Updated
Nov 23, 2025 - C#
Improve this page
Add a description, image, and links to the nozzle-design topic page so that developers can more easily learn about it.
Add this topic to your repo
To associate your repository with the nozzle-design topic, visit your repo's landing page and select "manage topics."