What is it about?
In this study we explore cavity-based scramjet combustion using numerical simulations and experiments. Good agreement between simulation results and experimental data is achieved. The combined set of results is used to analyze the cavity stabilization mechanism.
Featured Image
Read the Original
This page is a summary of: Large-Eddy Simulation of Supersonic Combustion in a Mach 2 Cavity Model Scramjet Combustor, AIAA Journal, January 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j064432.
You can read the full text:
Contributors
Be the first to contribute to this page
