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Updated: May 29, 2025

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

Lin Zhang1, Jianhan Liang2, Yi Wang3

  • 1Hypersonic Technology Laboratory, National University of Defense Technology, Changsha, 410073, Hunan, China. zhanglin11@nudt.edu.cn.

Scientific Reports
|February 5, 2025
PubMed

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