2015
DOI: 10.4271/2015-01-0795
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The Influence of Diesel End-of-Injection Rate Shape on Combustion Recession

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Cited by 19 publications
(10 citation statements)
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“…After the end of injection, the luminous combustion is seen to split into two parts, one short tail traveling upstream ("combustion recession") and a second tail, corresponding to burn out of the jet, traveling downstream. The progression of the luminous zone towards the injector is similar to the observations and analyses of previous studies, and can be interpreted as an ignition event [20,25,40,41].…”
Section: Oh* Chemiluminescencesupporting
confidence: 86%
“…After the end of injection, the luminous combustion is seen to split into two parts, one short tail traveling upstream ("combustion recession") and a second tail, corresponding to burn out of the jet, traveling downstream. The progression of the luminous zone towards the injector is similar to the observations and analyses of previous studies, and can be interpreted as an ignition event [20,25,40,41].…”
Section: Oh* Chemiluminescencesupporting
confidence: 86%
“…From this perspective, it can be seen that the RANS simulations well replicate the extents of combustion recession reactions seen in the experiments, and if multiple experimental realizations were available, the ensemble average of those realizations would appear more similar to the RANS simulations, with a more uniform distribution of OH* upstream of the LOL as combustion recession progresses. This general combustion recession sequence, including ignition of isolated pockets upstream of the LOL, followed by expansion and merging of the initial reaction regions, has also been observed in experiments of Knox et al 5 and Koci et al 9 for low ambient temperatures and low oxygen concentrations.…”
Section: Simulation Of Combustion Recessionsupporting
confidence: 66%
“…Recent experimental studies have shown that under negative ignition-dwell conditions, second-stage ignition may or may not occur in near-nozzle mixtures after EOI, depending jointly on the in-cylinder thermodynamic conditions and the magnitude and speed of the EOI entrainment wave. 511 When second-stage ignition occurs in mixtures upstream of the lifted diesel flame after EOI, this phenomenon has been termed “combustion recession.” Combustion recession can appear as either separated pockets of high-temperature reaction zones between the injector nozzle and the lifted diffusion flame position, or lift-off length (LOL), or as a rapid sequence of ignition reactions that travel back toward the injector nozzle. In contrast to “flash back,” 1 a term adopted in the gas turbine community for conditions where flames propagate back toward the fuel nozzle because of a mismatch in the local flame speed and fuel jet velocity, autoignition appears to drive combustion recession in diesel sprays.…”
Section: Introductionmentioning
confidence: 99%
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“…The extent to which second-stage ignition is able to recess toward the injector is different for the three injection timings. Similar combustion recession processes have been seen in other studies [25,28,[36][37][38] .…”
Section: Single-injection Experimental Resultssupporting
confidence: 73%