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September 1, 2003Journal of Propulsion and Power

Fuel Injection and Flame Stabilization in a Liquid-Kerosene-Fueled Supersonic Combustor

Yu Gong J. G. Li Xinyu Chang Li‐Hui Chen Chih‐Jen Sung

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Abstract

Investigations on combustion enhancement and stabilization of liquid kerosene using five different integrated fuel-injection/cavity-based flameholder configurations were conducted in a model combustor of cross sections 51 x 70 mm. The entry Mach number wa

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Cite This Study

Gong et al. (2003) studied this question.

synapsesocial.com/papers/6a0fc27dd13714ec96fe919c https://doi.org/10.2514/2.6179

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Synapse has enriched 5 closely related papers on similar clinical questions. Consider them for comparative context:

1Hydrocarbon-fueled scramjet combustor investigationOriginal Research · 1992 · 94 citations
2Flame-Holding Configurations for Kerosene Combustion in a Mach 1.8 AirflowOriginal Research · 1998 · 91 citations
3Effect of Flame-Holding Cavities on Supersonic-Combustion PerformanceOriginal Research · 2001 · 149 citations
4Supersonic Combustion Experiments with a Cavity-Based Fuel InjectorOriginal Research · 2001 · 309 citations
5Experimental Investigation on Flameholding Mechanism and Combustion Performance in Hydrogen-Fueled Supersonic CombustorsOriginal Research · 2002 · 39 citations

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