Show simple item record

contributor authorLing, Julia
contributor authorElkins, Christopher J.
contributor authorEaton, John K.
date accessioned2017-05-09T01:24:36Z
date available2017-05-09T01:24:36Z
date issued2015
identifier issn0889-504X
identifier otherturbo_137_07_071003.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/159939
description abstractTrailing edge slot film cooling is a widely used method of protecting the thin trailing edge of turbine blades from hot gas impingement. The structures that separate the slots, known as “lands,â€‌ come in a variety of configurations which can be broadly classified as either “taperedâ€‌ or “straight.â€‌ This paper examines the effect of the land taper angle on the mixing of the coolant flow with the main flow by comparing three configurations: a case with straight lands, a previously reported case with slightly tapered lands, and a case with strongly tapered lands. In each case, the slot width and the land width at the plane of the slot exit are kept constant. For each configuration, the mean volumetric coolant concentration distribution and threecomponent velocity field were measured using magnetic resonance imaging (MRI) techniques. It is shown that the land taper angle has a strong effect on the mean flow features and coolant surface effectiveness. Furthermore, the impact of the lands configuration on the flow field and concentration distribution is seen not just in the cutback region, but also in the wake of the blade.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Effect of Land Taper Angle on Trailing Edge Slot Film Cooling
typeJournal Paper
journal volume137
journal issue7
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4029174
journal fristpage71003
journal lastpage71003
identifier eissn1528-8900
treeJournal of Turbomachinery:;2015:;volume( 137 ):;issue: 007
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record