2015
DOI: 10.4271/2015-01-0796
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Experimental and Numerical Investigations of Close-Coupled Pilot Injections to Reduce Combustion Noise in a Small-Bore Diesel Engine

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Cited by 39 publications
(26 citation statements)
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“…Time-varied image distortion due to refraction at the curved surface of the window was corrected frame by frame with the ray-tracing analysis. 20 Flame images observed through the bottom window of the cavity and local temperature and KL factor (Soot concentration) distribution images analyzed by two-color method for conventional combustion with the single injector and ACCORDIC were compared in Figure 17. The luminous flame with the single injector was less than that with the multiple injectors after 15°A…”
Section: Combustion Observation By a Bottom-view Transparent Enginementioning
confidence: 99%
“…Time-varied image distortion due to refraction at the curved surface of the window was corrected frame by frame with the ray-tracing analysis. 20 Flame images observed through the bottom window of the cavity and local temperature and KL factor (Soot concentration) distribution images analyzed by two-color method for conventional combustion with the single injector and ACCORDIC were compared in Figure 17. The luminous flame with the single injector was less than that with the multiple injectors after 15°A…”
Section: Combustion Observation By a Bottom-view Transparent Enginementioning
confidence: 99%
“…The ignition delay and physical properties of conventional diesel fuel can be matched with this blend as reported by previous studies. 12,13 Combustion imaging setup A simultaneous high-speed flame natural luminosity imaging and OH* chemiluminescence imaging technique is developed to provide temporally and spatially resolved information about the ignition and the early combustion process. OH* chemiluminescence imaging was chosen for determining the high-temperature ignition because excited state species, such as OH*, are formed during the stoichiometric combustion of hydrocarbon fuels 14 and soot formation generally occurs right after the onset of high-temperature reactions.…”
Section: Experimental Apparatusmentioning
confidence: 99%
“…Shibata and colleagues 17,18 developed combustion noise simulation further and applied it to two-stage HTHR NCS combustion in 2016 and discussed the NCS combustion mechanism. Furthermore, Busch et al 19,20 reported the combustion noise reduction by short pilot-main injections and much research has been conducted with combustion noise spectrum analysis. The fuel penetration rate data provide evidence that rate shaping of the initial phase of the main injection is occurring in the engine and that this rate shaping is largely consistent with the injection rate data; however, the results demonstrate that these changes are not directly responsible for the observed trends in combustion noise.…”
Section: Introductionmentioning
confidence: 99%