What is it about?
3D simulations were conducted to investigate the vapor kerosene/air rotating detonation engines by an improving unstructured CE/SE method. The effects of the divergence section on flow field and RDE performance are analyzed.
Featured Image
Read the Original
This page is a summary of: Effects of Divergence Inlet on Kerosene/Air Rotating Detonation Engines, AIAA Journal, May 2022, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j061549.
You can read the full text:
Contributors
The following have contributed to this page