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

Abstract In order to investigate the acoustic oscillation characteristics of gas–liquid pintle rocket engines and elucidate the path by which spray combustion process provides energy to the combustor pressure oscillation, a LOX/GCH4 pintle engine with rectangular combustor was designed. By adding tr...

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Detalhes bibliográficos

Principais autores:	Xuan Jin, Chao Zhu, Dejiang Chen, Zhongpei Zhang
Formato:	Artigo
Idioma:	Inglês
Publicado em:	Nature Portfolio 2024-06-01
Colecção:	Scientific Reports
Assuntos:	LOX/GCH4 pintle engine Transverse velocity disturbance Acoustic response characteristic Transient spray combustion process Numerical simulation
Acesso em linha:	https://doi.org/10.1038/s41598-024-64027-2
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