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
Designing a ramjet engine using first principles of compressible flow. Components simulated include: inlet, diffuser, flameholder, combustor, converging and diverging nozzle.
End-to-end simulation of a guided 155mm Ramjet projectile. Integrates high-fidelity ANSYS Fluent CFD (Mach 2.0) with a custom Python 6-DOF flight dynamics engine and Proportional Navigation (PN) control loop for precision target intercept.
Add a description, image, and links to the ramjet topic page so that developers can more easily learn about it.
To associate your repository with the ramjet topic, visit your repo's landing page and select "manage topics."