Show simple item record

contributor authorSingh, Kuldeep
contributor authorPremachandran, B.
contributor authorRavi, M. R.
date accessioned2019-02-28T11:01:31Z
date available2019-02-28T11:01:31Z
date copyright5/25/2018 12:00:00 AM
date issued2018
identifier issn0022-1481
identifier otherht_140_09_094504.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4251843
description abstractIn this work, a numerical study is conducted to investigate film cooling of a corrugated surface. A conjugate heat transfer analysis is carried out, accounting for the presence of thermal barrier coating (TBC) and gas radiation. The Mach number of mainstream flow is maintained at Ma = 0.6, while cold stream Mach number is varied from 0.3 to 0.58, and density ratio is kept 4. From this study, it is observed that the overall film cooling effectiveness increases by a value ranging from 0.10 to 0.15 with the use of TBC. The hot side metallic wall temperature increases in the range of 100–150 °C when the effect of gas radiation is considered. It is also found that the film cooling effectiveness decreases with decrease in the cold side Mach number.
publisherThe American Society of Mechanical Engineers (ASME)
titleEffect of Thermal Barrier Coating and Gas Radiation on Film Cooling of a Corrugated Surface
typeJournal Paper
journal volume140
journal issue9
journal titleJournal of Heat Transfer
identifier doi10.1115/1.4039761
journal fristpage94504
journal lastpage094504-5
treeJournal of Heat Transfer:;2018:;volume( 140 ):;issue: 009
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record