The effect of kerosene injection on ignition probability of local ignition in a scramjet combustor
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference13 articles.
1. Experimental investigation of ignition transient phase in model supersonic combustor;Xi;J. Aerosp. Eng.,2014
2. Investigation of kerosene combustion characteristics with pilot hydrogen in model supersonic combustors;Yu;J. Propuls. Power,2001
3. Experimental investigation of combustion mechanisms of kerosene-fueled scramjet engines with double-cavity flameholders;Pan;Acta Mech. Sin.,2011
4. Plasma-assisted ignition for a kerosene fueled scramjet at mach 1.8;Li;Aerosp. Sci. Technol.,2013
5. Effect of cavity configuration on kerosene spark ignition in a scramjet combustor at ma 4.5 flight condition;Bao;Acta Astronaut.,2015
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3. Experimental study on the penetration and evaporation characteristics of a liquid kerosene jet in the supersonic crossflow;Physics of Fluids;2024-07-01
4. Effect of upstream injection on local flame intensity in a scramjet combustor fueled with liquid kerosene at Mach 4 flight condition;Aerospace Science and Technology;2024-05
5. Effect of Local Equivalent Ratio on Spark Ignition Characteristics in a Kerosene Scramjet Combustor at Mach 4 Flight Condition;2024
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