Injection angles on flow structures and mixing properties in a supersonic combustor at low Mach crossflow

Zhang L, Liang J, Wang Y, Zhao W, Yang L.

DOI: 10.21203/rs.3.rs-5145975/v1
Published: 2024-11-28
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Cite this work

BibTeX

@article{allodium:10.21203/rs.3.rs-5145975/v1,
  title = {Injection angles on flow structures and mixing properties in a supersonic combustor at low Mach crossflow},
  author = {Zhang L and  Liang J and  Wang Y and  Zhao W and  Yang L.},
  year = {2024},
  doi = {10.21203/rs.3.rs-5145975/v1},
  url = {https://doi.org/10.21203/rs.3.rs-5145975/v1}
}

RIS

TY  - JOUR
TI  - Injection angles on flow structures and mixing properties in a supersonic combustor at low Mach crossflow
AU  - Zhang L
AU  -  Liang J
AU  -  Wang Y
AU  -  Zhao W
AU  -  Yang L.
PY  - 2024
DO  - 10.21203/rs.3.rs-5145975/v1
UR  - https://doi.org/10.21203/rs.3.rs-5145975/v1
ER  -

APA

L, Z., J, L., Y, W., W, Z., & L., Y. (2024). Injection angles on flow structures and mixing properties in a supersonic combustor at low Mach crossflow. https://doi.org/10.21203/rs.3.rs-5145975/v1

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europe-pmc · retrieved 2026-11-10T14:07:35.173Z