Low Reynolds number flow over a plane symmetric sudden expansion

Author:

Durst F.,Melling A.,Whitelaw J. H.

Abstract

Flow visualization and laser-anemometry measurements are reported in the flow downstream of a plane 3: 1 symmetric expansion in a duct with an aspect ratio of 9·2: 1 downstream of the expansion. The flow was found to be markedly dependent on Reynolds number, and strongly three-dimensional even well away from the channel corners except at the lowest measurable velocities. The measurements at a Reynolds number of 56 indicated that the separation regions behind each step were of equal length. Symmetric velocity profiles existed from the expansion to a fully developed, parabolic profile far downstream, although there were substantial three-dimensional effects in the vicinity of the separation regions. The velocity profiles were in good agreement with those obtained by solving the two-dimensional momentum equation. At a Reynolds number of 114, the two separation regions were of different lengths, leading to asymmetric velocity profiles; three dimensional effects were much more pronounced. At a Reynolds number of 252, a third separation zone was found on one wall, downstream of the smaller of the two separation zones adjacent to the steps. As at the lower Reynolds numbers, the flow was very stable. At higher Reynolds numbers the flow became less stable and periodicity became increasingly important in the main stream; this was accompanied by a highly disturbed fluid motion in the separation zones, as the flow tended towards turbulence.

Publisher

Cambridge University Press (CUP)

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference12 articles.

1. Sato H. 1959 Further investigation on the transition of two-dimensional separated layer at subsonic speeds. J. Phys. Soc. Japan,14,1797.

2. Zemanick, P. P. & Dougall R. S. 1970 Local heat transfer downstream of an abrupt circular channel expansion.J. Heat Transfer, Trans. A.S.M.E. C92,53.

3. Iribarne A. , Frantisak F. , Hummel, R. L. & Smith J. W. 1972 An experimental study of instabilities and other flow properties of alaminar pipe jet. A.1.Ch.E. J.,18,689.

4. Sato H. 1956 Experimental investigation on the transition of laminar separated flow. J. Phys. Soc. Japan,11,702.

5. Gosman A. D. , Pun W. M. , Runchal A. K. , Spalding, D. B. & Wolfshtein M. 1969 Heat and Mass Transfer in Recirculating Flows. Academic.

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3