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...
Saved in:
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!
|
Similar Items
-
Numerical Study on Effects of Arrayed Pulsed Energy Depositions on a Supersonic Combustor
by: Zilin Cai, et al.
Published: (2022-01-01) -
Suppression of Supersonic Cavity Oscillations Using Pulsed Upstream Mass Injection
by: Weipeng Li
Published: (2016-01-01) -
The analysis of the influence of the turbulence model selection on the parameters of interaction of a supersonic jet with an obstacle
by: R. A. Peshkov, et al.
Published: (2024-10-01) -
Perfecting of methods of supersonic inspection and structureskopy of foundry production in auto- and tractor-building
by: P. P. Prokhorenko, et al.
Published: (2002-02-01) -
Wind Tunnel Testing on Start/Unstart Characteristics of Finite Supersonic Biplane Wing
by: Hiroshi Yamashita, et al.
Published: (2013-01-01)