Influence of Buoyancy and Inter-Surface Radiation on Confined Jet Impingement Cooling of a Semi-Cylindrical Concave Plate

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dc.authoridSARPER, BUGRA/0000-0001-7554-6575
dc.contributor.authorSarper, Bugra
dc.date.accessioned2025-03-17T12:25:35Z
dc.date.available2025-03-17T12:25:35Z
dc.date.issued2024
dc.departmentTarsus Üniversitesi
dc.description.abstractIn this article, the confined jet impingement cooling of a semicylindrical concave plate is analyzed numerically. The finite volume approach is applied to two-dimensional numerical simulations in the transient regime. Air is employed as the working fluid and is regarded as nonparticipant for radiation. The investigation is done for different jet Reynolds numbers ( Re j) ranging from 100 to 1000, as the Richardson number ( Ri) corresponding to this interval ranges between 0.1 and 10. For any Richardson number, the modified Grashof number ( Gr *) is fixed at 105. When analyzing the impact of intersurface radiation between the target plate and confined surfaces on the overall cooling performance, three emissivity values ( epsilon = 0.05, 0.5, and 0.95) are taken into consideration. Additionally, simulations are done for the pure convective heat transfer, ignoring intersurface radiation ( epsilon = 0.0). The influence of surface emissivity and the Richardson number on velocity, temperature, and pressure distribution in the flow domain, local dimensionless temperature ( theta) alterations on the target plate and confined walls, alterations in convective ( Nu c ), radiative ( Nu r ), overall Nusselt numbers ( Nu ovr ), pressure coefficient ( C p), and ratio of radiative Nusselt number to overall Nusselt number ( Nu r / Nu ovr) on the target plate are highlighted. The findings demonstrate that surface emissivity has a significant influence on thermal and hydrodynamic boundary layer formation, buoyancy induced flow and heat transfer, and the proportion of intersurface radiation in overall heat transfer rises as the Richardson number and surface emissivity increase. At low Richardson numbers, the pressure in the stagnation region is greater than the atmospheric pressure. However, as the buoyancy effect increases, the pressure in the stagnation region falls below the atmospheric pressure and rises toward the exit.
dc.identifier.doi10.1115/1.4064038
dc.identifier.issn2832-8450
dc.identifier.issn2832-8469
dc.identifier.issue3
dc.identifier.scopus2-s2.0-85180405534
dc.identifier.scopusqualityQ2
dc.identifier.urihttps://doi.org/10.1115/1.4064038
dc.identifier.urihttps://hdl.handle.net/20.500.13099/1771
dc.identifier.volume146
dc.identifier.wosWOS:001154954900008
dc.identifier.wosqualityN/A
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.institutionauthorSarper, Bugra
dc.language.isoen
dc.publisherAsme
dc.relation.ispartofAsme Journal of Heat and Mass Transfer
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.snmzKA_WOS_20250316
dc.subjectjet impingement
dc.subjectconvection
dc.subjectlaminar
dc.subjectinter-surface radiation
dc.subjectbuoyancy
dc.subjectemissivity
dc.titleInfluence of Buoyancy and Inter-Surface Radiation on Confined Jet Impingement Cooling of a Semi-Cylindrical Concave Plate
dc.typeArticle

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