Turbulent boundary layers over sparsely-spaced rod-roughened walls
DC Field | Value | Language |
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dc.contributor.author | Nadeem, Muhammad | ko |
dc.contributor.author | Lee, Jae Hwa | ko |
dc.contributor.author | Lee, Jin | ko |
dc.contributor.author | Sung, Hyung Jin | ko |
dc.date.available | 2015-09-01T06:01:50Z | - |
dc.date.created | 2015-07-08 | ko |
dc.date.issued | 2015-12 | ko |
dc.identifier.citation | INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, v.56, pp.16 - 27 | ko |
dc.identifier.issn | 0142-727X | ko |
dc.identifier.uri | https://scholarworks.unist.ac.kr/handle/201301/16425 | - |
dc.description.abstract | Direct numerical simulations (DNSs) of spatially developing turbulent boundary layers (TBLs) over sparsely-spaced two-dimensional (2D) rod-roughened walls were performed. The rod elements were periodically arranged along the streamwise direction with pitches of p(x)/k = 8, 16, 32, 64 and 128, where p(x) is the streamwise spacing of the rods, and k is the roughness height. The Reynolds number based on the momentum thickness was varied from Re-0 = 300-1400, and the height of the roughness element was k = 1.5 theta(in), where theta(in), is the momentum thickness at the inlet. The characteristics of the TBLs, such as the friction velocity, mean velocity, and Reynolds stresses over the rod-roughened walls, were examined by varying the spacing of the roughness features (8 <= p(x)/k <= 128). The outer-layer similarity between the rough and smooth walls was established for the sparsely-distributed rough walls (p(x)/k >= 32) based on the profiles of the Reynolds stresses, whereas those are not for p(x)/k = 8 and 16. Inspection of the interaction between outer-layer large-scale motions and near-wall small-scale motions using two-point amplitude modulation (AM) covariance showed that modulation effect of large-scale motions on near-wall small-scale motions was strongly disturbed over the rough wall for p(x)/k = 8 and 16. For p(x)/k >= 32, the flow that passed through the upstream roughness element transitioned to a smooth wall flow between the consecutive rods. The strong influence of the surface roughness in the outer layer for p(x)/k = 8 and 16 was attributed to large-scale erupting motions by the surface roughness, creating both upward shift of the near-wall turbulent energy and active energy production in the outer layer with little influence on the near-wall region. ess, creating both upward shift of the near-wall turbulent energy and active energy production in the outer layer with little influence on the near-wall region. | ko |
dc.description.statementofresponsibility | close | - |
dc.language | 영어 | ko |
dc.publisher | ELSEVIER SCIENCE INC | ko |
dc.title | Turbulent boundary layers over sparsely-spaced rod-roughened walls | ko |
dc.type | ARTICLE | ko |
dc.identifier.scopusid | 2-s2.0-84937573051 | ko |
dc.identifier.wosid | 000366961900002 | ko |
dc.type.rims | ART | ko |
dc.description.wostc | 0 | * |
dc.description.scopustc | 0 | * |
dc.date.tcdate | 2016-01-21 | * |
dc.date.scptcdate | 2015-11-04 | * |
dc.date.scptcdate | 2015-11-04 | * |
dc.identifier.doi | 10.1016/j.ijheatfluidflow.2015.06.006 | ko |
dc.identifier.url | http://www.sciencedirect.com/science/article/pii/S0142727X15000715 | ko |
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