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contributor authorV. Scherer
contributor authorS. Wittig
date accessioned2017-05-08T23:35:36Z
date available2017-05-08T23:35:36Z
date copyrightJanuary, 1991
date issued1991
identifier issn1528-8919
identifier otherJETPEZ-26683#126_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/108580
description abstractConvective heat transfer is examined in two typical examples of separated flows, namely, the flow over a backward-facing step and a two-dimensional jet entering a crossflow. Local Nusselt numbers were determined in and behind the recirculation region. The main parameters influencing the heat transfer, the Reynolds number, and the momentum flux ratio of the jet and the crossflow have been varied over a wide range. In addition to heat transfer measurements, the flow field has been documented using an LDA system and oil film technique. The static pressure distribution at the wall within the separated flow is also given. The measurements are compared with the results of a numerical code, based on a finite volume method, where the well known k-ε model is employed. The differences in Nusselt numbers predicted with one- and two-layer models are shown to demonstrate the influence of wall functions on heat transfer. The numerical and experimental results are compared with available data, and the differences and similarities in the heat transfer behavior of separated flows are discussed.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Influence of the Recirculation Region: A Comparison of the Convective Heat Transfer Downstream of a Backward-Facing Step and Behind a Jet in a Crossflow
typeJournal Paper
journal volume113
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2906520
journal fristpage126
journal lastpage134
identifier eissn0742-4795
keywordsFoundry coatings
keywordsConvection
keywordsFlow (Dynamics)
keywordsHeat transfer
keywordsMeasurement
keywordsReynolds number
keywordsFinite volume methods
keywordsFunctions
keywordsLaser Doppler anemometry
keywordsPressure AND Momentum
treeJournal of Engineering for Gas Turbines and Power:;1991:;volume( 113 ):;issue: 001
contenttypeFulltext


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