2003
DOI: 10.1007/s00231-002-0335-6
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Local heat transfer from a hot plate to a water jet

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Cited by 35 publications
(17 citation statements)
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“…4 presents the boiling curves of wall heat flux versus temperature at x = 0. The transient boiling curve obtained from the DNS of quenching process matches well with the steady-state boiling curve obtained from the previous DNS study [24] under the constant wall temperature conditions, which is comparable to the experimental data of Robidou et al [3,4]. This is not consistent with the experimental observation reported in the literature [6][7][8][9][10][11] that the transient boiling curve has an initial boiling regime where the wall heat flux increases rapidly with decreasing wall temperature.…”
Section: Resultssupporting
confidence: 84%
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“…4 presents the boiling curves of wall heat flux versus temperature at x = 0. The transient boiling curve obtained from the DNS of quenching process matches well with the steady-state boiling curve obtained from the previous DNS study [24] under the constant wall temperature conditions, which is comparable to the experimental data of Robidou et al [3,4]. This is not consistent with the experimental observation reported in the literature [6][7][8][9][10][11] that the transient boiling curve has an initial boiling regime where the wall heat flux increases rapidly with decreasing wall temperature.…”
Section: Resultssupporting
confidence: 84%
“…The solid properties are varied as (ρc p ) s = 5 × 10 4 ∼ 5 × 10 6 J/m 3 K and λ s = 11 ∼ 44 W/mK to investigate their effects on the quenching process. We choose a nozzle width of W j = 1 mm, a jet velocity of V j = 0.8 m/s, a jet subcooling of T sat − T j = 16°C and an initial solid superheat of ΔT s,i = 400°C or 500°C, based on the experimental conditions of Robidou et al [3,4]. The computational domain is taken to be a two-dimensional region, as depicted in Fig.…”
Section: Resultsmentioning
confidence: 99%
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“…The surface heat flux curves are sharper and with higher peak for Re = 24,000, as compared to the wider curves with lower peak at Re = 5000. For a certain jet diameter, the effect of jet Reynolds number on surface cooling and heat flux can be attributed by [36][37][38][39]. This 'shoulder of flux' is due to periodic bubble oscillation at the hot wall surface due to hydrodynamic fragmentation of vapor spots by the jet.…”
Section: Effect Of Jet Reynolds Numbermentioning
confidence: 99%
“…Further, it has been recognized that the heat transfer during water cooling varies at the cooled surface in space and time [23,24]. In a number of publications two-dimensional inverse heat conduction model are used to identify heat flux and heat transfer coefficient [25][26][27][28][29]. Jha et al [27] and Sarkar et al [28] have assumed some simplifications such as adiabatic conditions at the surfaces that are not being cooled by jet impingement.…”
Section: Introductionmentioning
confidence: 99%