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contributor authorT. A. Trabold
contributor authorN. T. Obot
date accessioned2017-05-08T23:26:00Z
date available2017-05-08T23:26:00Z
date copyrightOctober, 1987
date issued1987
identifier issn0889-504X
identifier otherJOTUEI-28586#594_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/103204
description abstractAn experimental investigation was carried out to determine the effects of jet-induced crossflow on impingement heat transfer from rough surfaces. The jets impinged on surfaces having repeated square ribs, with transverse flow of the spent air. Two crossflow schemes were tested: discharge of the spent air through two opposite sides (intermediate crossflow) and through one side (complete or maximum crossflow) of the rectangular impingement surface. The rib height was fixed at 0.813 mm, while the pitch-to-height ratio (p /e) was varied between 6 and 10. The study covered standoff spacing and jet Reynolds number in the range 2 to 16 jet hole diameters and 1300 to 21,000, respectively. Three nozzle plates, having 48, 90, and 180 square-edged holes, were tested. For the maximum crossflow scheme, the presence of roughness results in small upstream reductions in heat transfer coefficient, with marked improvement in the downstream section; indicating that roughness elements can be used to compensate for the degradation that is usually associated with impingement on smooth surfaces.
publisherThe American Society of Mechanical Engineers (ASME)
titleImpingement Heat Transfer Within Arrays of Circular Jets: Part II—Effects of Crossflow in the Presence of Roughness Elements
typeJournal Paper
journal volume109
journal issue4
journal titleJournal of Turbomachinery
identifier doi10.1115/1.3262153
journal fristpage594
journal lastpage601
identifier eissn1528-8900
treeJournal of Turbomachinery:;1987:;volume( 109 ):;issue: 004
contenttypeFulltext


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