2014
DOI: 10.1016/j.ast.2014.08.017
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Structural design and performance experiment of a single vortex combustor with single-cavity and air blast atomisers

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Cited by 30 publications
(2 citation statements)
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“…The values (CO), (fuel), and (NOX) are calculated on the base of 15% percent oxygen. The combustion efficiency is calculated by determining the heat loss at the combustor outlet via the incomplete combustion products [67].…”
Section: Post-processing Methodmentioning
confidence: 99%
“…The values (CO), (fuel), and (NOX) are calculated on the base of 15% percent oxygen. The combustion efficiency is calculated by determining the heat loss at the combustor outlet via the incomplete combustion products [67].…”
Section: Post-processing Methodmentioning
confidence: 99%
“…A new method using a plasma jet igniter was developed and applied in the integrated afterburner by Fei et al [13] to reduce ignition delay time and achieve stable combustion. In addition, adopting new stabilization structures, such as the cavity flameholder instead of the traditional bluff-body flameholder, has also become one of the research directions concerning the integrated afterburner in recent years [14][15][16]. The cavity flameholder is based on the mechanism of the trapped vortex and is more appropriate for high-speed conditions [17].…”
Section: Introductionmentioning
confidence: 99%