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Updated: Jun 24, 2025

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Transient spray combustion characteristics in a gas-liquid pintle rocket engine under acoustic excitation

Xuan Jin1,2, Chao Zhu3,4, Dejiang Chen5,6

  • 1Hypervelocity Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang, 621000, China. 1540445629@qq.com.

Scientific Reports
|June 7, 2024
PubMed

Keywords:
Acoustic response characteristicLOX/GCH4 pintle engineNumerical simulationTransient spray combustion processTransverse velocity disturbance

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