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

  1. Lin Zhang
  2. Jianhan Liang
  3. Yi Wang
  4. Wei Zhao
  5. Leichao Yang
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  1. Version published to 10.1038/s41598-025-88987-1
  2. Version published to 10.21203/rs.3.rs-5145975/v1 on Research Square