Please use this identifier to cite or link to this item: http://hdl.handle.net/11452/31195
Title: Experimental investigation of impingement heat transfer from a round rib-roughened surface
Authors: İsman, Mustafa Kemal
Uludağ Üniversitesi/Mühendislik Mimarlık Fakültesi/Makine Mühendisliği Bölümü.
Can, Muhiddin
7006114954
Keywords: Thermodynamics
Mechanics
Flow structure
Mass-transfer
Jet
Fighter aircraft
Reynolds number
Nusselt number
Experimental investigations
Impingement heat transfer
Impinging jet
Low speed
Roughened surfaces
Spot cooling
Stagnation points
Heat transfer
Issue Date: 29-Aug-2016
Publisher: Springer
Citation: İsman, M. K. ve Can, M. (2017). ''Experimental investigation of impingement heat transfer from a round rib-roughened surface''. Heat and Mass Transfer/Waerme- und Stoffuebertragung, 53(4), 1405-1412.
Abstract: An experimental investigation on impingement heat transfer from a rib-roughened surface is performed. Single, double, and triple rib configurations are tested. The rib is also located at three different positions for a single rib case. The Reynolds number is varied from 10,000 to 50,000 whereas the dimensionless jet-to-surface distance (z/D) is kept constant as 8. Results show that, the Nusselt number decreases just before a rib. After the rib, however, the Nusselt number decreases by a larger amount. Since ribs cause a reincreasing in the Nusselt number after the stagnation point and since the stagnation point Nusselt number is not affected by ribs, they can be used to enhance heat transfer especially for spot cooling applications. It is also obtained that using ribs is more useful for low speed impinging jets, when heat transfer from the whole surface is considered.
URI: https://doi.org/10.1007/s00231-016-1911-5
https://link.springer.com/article/10.1007/s00231-016-1911-5
http://hdl.handle.net/11452/31195
ISSN: 0947-7411
1432-1181
Appears in Collections:Scopus
Web of Science

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