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...
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Main Authors: | , , , , |
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Format: | Article |
Language: | English |
Published: |
Nature Portfolio
2025-02-01
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Series: | Scientific Reports |
Online Access: | https://doi.org/10.1038/s41598-025-88987-1 |
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