File Download

There are no files associated with this item.

  • Find it @ UNIST can give you direct access to the published full text of this article. (UNISTARs only)
Related Researcher

이재화

Lee, Jae Hwa
Flow Physics and Control Lab.
Read More

Views & Downloads

Detailed Information

Cited time in webofscience Cited time in scopus
Metadata Downloads

Skin-friction drag reduction in turbulent channel flow based on streamwise shear control

Author(s)
Kim, Jung HoonLee, Jae Hwa
Issued Date
2017-02
DOI
10.1016/j.ijheatfluidflow.2016.12.001
URI
https://scholarworks.unist.ac.kr/handle/201301/21050
Fulltext
http://www.sciencedirect.com/science/article/pii/S0142727X16302016
Citation
INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, v.63, pp.28 - 43
Abstract
It is known that stretching and intensification of a hairpin vortex by mean shear play an important role to create a hairpin vortex packet, which generates the large Reynolds shear stress associated with skin-friction drag in wall-bounded turbulent flows. In order to suppress the mean shear at the wall for high efficient drag reduction (DR), in the present study, we explore an active flow control concept using streamwise shear control (SSC) at the wall. The longitudinal control surface is periodically spanwise-arranged with no-control surface while varying the structural spacing, and an amplitude parameter for imposing the strength of the actuating streamwise velocity at the wall is introduced to further enhance the skin-friction DR. Significant DR is observed with an increase in the two parameters with an accompanying reduction of the Reynolds stresses and vorticity fluctuations, although a further increase in the parameters amplifies the turbulence activity in the near-wall region. In order to study the direct relationship between turbulent vortical structures and DR under the SSC, temporal evolution with initial eddies extracted by conditional averages for Reynolds-stress-maximizing Q2 events are examined. It is shown that the generation of new vortices is dramatically inhibited with an increase in the parameters throughout the flow, causing fewer vortices to be generated under the control. However, when the structural spacing is sufficiently large, the generation of new vortex is not suppressed over the no-control surface in the near-wall region, resulting in an increase of the second- and fourth-quadrant Reynolds shear stresses. Although strong actuating velocity intensifies the near-wall turbulence, the increase in the turbulence activity is attributed to the generation of counter-clockwise near-wall vortices by the increased vortex transport.
Publisher
ELSEVIER SCIENCE INC
ISSN
0142-727X
Keyword (Author)
Turbulent boundary layerDirect numerical simulationDrag reductionTurbulent structure
Keyword
NEAR-WALL TURBULENCEBOUNDARY-LAYERSUPERHYDROPHOBIC SURFACESVELOCITYPACKETS

qrcode

Items in Repository are protected by copyright, with all rights reserved, unless otherwise indicated.