Ignition enhancement of liquid kerosene by a novel high-energy spark igniter in scramjet combustor at Mach 4 flight condition
Author:
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference28 articles.
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2. Review of cavity ignition in supersonic flows;Zun;Acta Astronaut.,2019
3. Combustion characteristics of a dual-mode scramjet combustor with cavity flameholder;Micka;Proc. Combust. Inst.,2009
4. Mixing and combustion characteristics of kerosene in a model supersonic combustor;Kumaran;J. Propuls. Power,2009
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1. Effect of local equivalent ratio on spark ignition characteristics in a kerosene scramjet combustor at Mach 4 flight condition;Aerospace Science and Technology;2024-10
2. 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
3. Numerical Study of High-Energy Spark Ignition Characteristics in a Scramjet Combustor;2024
4. Effect of Local Equivalent Ratio on Spark Ignition Characteristics in a Kerosene Scramjet Combustor at Mach 4 Flight Condition;2024
5. Investigation of ignition and flame propagation in an axisymmetric supersonic combustor with laser-induced plasma;Physics of Fluids;2023-12-01
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