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contributor authorSaha, Krishnendu
contributor authorAcharya, Sumanta
date accessioned2017-05-09T01:03:13Z
date available2017-05-09T01:03:13Z
date issued2013
identifier issn0889-504X
identifier otherturb_135_3_031028.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/153350
description abstractThe pressure drop and heat transfer in a two pass internal cooling channel with two different bend geometries is experimentally studied with the goal of improving the thermal performance factor (TPF) in the coolant channel. The geometries studied are (1) a baseline Ubend geometry with a rectangular divider wall, (2) a symmetrical bulb at the end of the divider wall, and (3) a combination of the symmetrical bulb and a bow on the opposite outer wall leading to a shaped flow contraction and expansion in the bend. Tests are conducted for four Reynolds number ranging from 10,000 to 55,000. The symmetrical bulb eliminates the separation due to the sharp turn and makes the heat transfer distribution in the bend portion more uniform. This modification reduces the bend pressure drop by 37% and augments the TPF by nearly 29% compared to the baseline case. The combination of bulb and bow case increases the local heat transfer in the bend region significantly, and reduces the bend pressure drop by nearly 27% leading to an augmentation of the TPF of 32% compared to the baseline case. These improvements in TPF point to the benefits of using the improved bend designs in internal cooling channels.
publisherThe American Society of Mechanical Engineers (ASME)
titleBend Geometries in Internal Cooling Channels for Improved Thermal Performance
typeJournal Paper
journal volume135
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4007582
journal fristpage31028
journal lastpage31028
identifier eissn1528-8900
treeJournal of Turbomachinery:;2013:;volume( 135 ):;issue: 003
contenttypeFulltext


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