Influence of injection angles on flow structures and mixing properties in a supersonic combustor at low Mach supersonic crossflow

Abstract The fuel-air mixing is of paramount importance in hypersonic air-breathing vehicles, and its performance is closely related to the fuel injection angle. This article presents an investigation into the influence of the injection angles on the flow and mixing processes in a supersonic combust...

Full description

Saved in:
Bibliographic Details
Main Authors: Lin Zhang, Jianhan Liang, Yi Wang, Wei Zhao, Leichao Yang
Format: Article
Language:English
Published: Nature Portfolio 2025-02-01
Series:Scientific Reports
Online Access:https://doi.org/10.1038/s41598-025-88987-1
Tags: Add Tag
No Tags, Be the first to tag this record!