2021
DOI: 10.1080/13647830.2021.1937702
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A detailed modelling on spray atomisation and combustion of LOX/GCH4 in variable area pintle injector rocket engines

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Cited by 7 publications
(1 citation statement)
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“…Particularly, Heister held that pintle engines require a higher degree of integrated design of the pintle injector and the combustion chamber than other types of rocket engines [6]. Currently, most investigations are devoted to the atomization characteristics [7][8][9][10][11][12][13] and combustion performance of pintle injectors [14][15][16][17][18], so further investigations are required on the thermal protection and ablation-induced problems. Especially for cryogenic bipropellants such as liquid oxygen (LOX)/liquid hydrogen (LH2) and LOX/liquid methane (LCH4), the pintle tip ablation cannot be ignored.…”
Section: Introductionmentioning
confidence: 99%
“…Particularly, Heister held that pintle engines require a higher degree of integrated design of the pintle injector and the combustion chamber than other types of rocket engines [6]. Currently, most investigations are devoted to the atomization characteristics [7][8][9][10][11][12][13] and combustion performance of pintle injectors [14][15][16][17][18], so further investigations are required on the thermal protection and ablation-induced problems. Especially for cryogenic bipropellants such as liquid oxygen (LOX)/liquid hydrogen (LH2) and LOX/liquid methane (LCH4), the pintle tip ablation cannot be ignored.…”
Section: Introductionmentioning
confidence: 99%