2022
DOI: 10.1016/j.applthermaleng.2022.118595
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Computational assessment of effects of throat diameter on combustion and turbulence characteristics in a pre-chamber engine

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Cited by 49 publications
(30 citation statements)
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“…The 3D contours reveal that, although the PCs have 12 nozzles, it mostly relies on the major activity of 6 bottom nozzles. Silva et al [21] discussed this unusual behavior, which is a combination of high-speed flow along the throat, followed by transonic flow at the top nozzle location, which prevents the comparable behavior to the bottom nozzles. Moreover, a major distinction in the jet topologies is observed; while G-Equation shows small jet exiting the top nozzles, the MZ-WSR only manifests the six bottom nozzle jets.…”
Section: Resultsmentioning
confidence: 99%
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“…The 3D contours reveal that, although the PCs have 12 nozzles, it mostly relies on the major activity of 6 bottom nozzles. Silva et al [21] discussed this unusual behavior, which is a combination of high-speed flow along the throat, followed by transonic flow at the top nozzle location, which prevents the comparable behavior to the bottom nozzles. Moreover, a major distinction in the jet topologies is observed; while G-Equation shows small jet exiting the top nozzles, the MZ-WSR only manifests the six bottom nozzle jets.…”
Section: Resultsmentioning
confidence: 99%
“…𝑢 ′ , was obtained from the transport equation for the turbulent kinetic energy (k) under the assumption of homogeneous and isotropic turbulence. Additional discussion can be found in previous works [21].…”
Section: Figure 1: Engine Fluid Domain (Adapted [21])mentioning
confidence: 95%
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