Show simple item record

contributor authorK. Kim
contributor authorM. E. Crawford
date accessioned2017-05-09T00:03:43Z
date available2017-05-09T00:03:43Z
date copyrightJanuary, 2000
date issued2000
identifier issn0889-504X
identifier otherJOTUEI-28673#78_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/124515
description abstractThe presence of wake-passing in the gas turbine environment significantly modifies the heat transfer characteristics on the downstream blade surface by causing wake-induced transition. In this study, time-dependent boundary layer calculations were carried out using a model for wake-induced transition based on a prescribed time-dependent intermittent function. The model is determined from the well-known turbulent spot propagation theory in a time-space diagram and from experimental evidence in the ensemble-averaged sense. Time-averaged heat transfer distributions are evaluated and compared with experimental results for different flow and wake-generating conditions over a flat plate. Comparison showed that the present time-dependent calculations yield more accurate results than existing steady superposition models. [S0889-504X(00)00901-6]
publisherThe American Society of Mechanical Engineers (ASME)
titlePrediction of Transitional Heat Transfer Characteristics of Wake-Affected Boundary Layers
typeJournal Paper
journal volume122
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.555430
journal fristpage78
journal lastpage87
identifier eissn1528-8900
keywordsTurbulence
keywordsWakes
keywordsBoundary layers
keywordsFlow (Dynamics)
keywordsHeat transfer
keywordsMeasurement AND Strips
treeJournal of Turbomachinery:;2000:;volume( 122 ):;issue: 001
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record