Drag Reduction in Turbulent Boundary Layers with Half Wave Wall Oscillations

Spatial square waves with positive cycle are used as steady forcing technique to study drag reduction effects on a turbulent boundary layer flow. Pseudospectral method is used for performing direct numerical simulations on very high resolution grids. A smooth step function is employed to prevent Gib...

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Main Authors: Mishra, Maneesh, Skote, Martin
Other Authors: School of Mechanical and Aerospace Engineering
Format: Article
Language:English
Published: 2015
Online Access:https://hdl.handle.net/10356/104296
http://hdl.handle.net/10220/38819
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-1042962023-03-04T17:20:41Z Drag Reduction in Turbulent Boundary Layers with Half Wave Wall Oscillations Mishra, Maneesh Skote, Martin School of Mechanical and Aerospace Engineering Spatial square waves with positive cycle are used as steady forcing technique to study drag reduction effects on a turbulent boundary layer flow. Pseudospectral method is used for performing direct numerical simulations on very high resolution grids. A smooth step function is employed to prevent Gibbs phenomenon at the sharp discontinuities of a square wave. The idea behind keeping only the positive cycle of the spatial forcing is to reduce the power consumption to boost net power savings. For some spatial frequency of the oscillations with half waves, it is possible to prevent recovery of skin friction back to the reference case values. A set of wall oscillation parameters is numerically simulated to study its effect on the power budget. Published version 2015-10-21T06:25:56Z 2019-12-06T21:30:00Z 2015-10-21T06:25:56Z 2019-12-06T21:30:00Z 2015 2015 Journal Article Mishra, M., & Skote, M. (2015). Drag Reduction in Turbulent Boundary Layers with Half Wave Wall Oscillations. Mathematical Problems in Engineering, 2015, 253249-. https://hdl.handle.net/10356/104296 http://hdl.handle.net/10220/38819 10.1155/2015/253249 194022 en Mathematical Problems in Engineering © 2015 Maneesh Mishra and Martin Skote. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
description Spatial square waves with positive cycle are used as steady forcing technique to study drag reduction effects on a turbulent boundary layer flow. Pseudospectral method is used for performing direct numerical simulations on very high resolution grids. A smooth step function is employed to prevent Gibbs phenomenon at the sharp discontinuities of a square wave. The idea behind keeping only the positive cycle of the spatial forcing is to reduce the power consumption to boost net power savings. For some spatial frequency of the oscillations with half waves, it is possible to prevent recovery of skin friction back to the reference case values. A set of wall oscillation parameters is numerically simulated to study its effect on the power budget.
author2 School of Mechanical and Aerospace Engineering
author_facet School of Mechanical and Aerospace Engineering
Mishra, Maneesh
Skote, Martin
format Article
author Mishra, Maneesh
Skote, Martin
spellingShingle Mishra, Maneesh
Skote, Martin
Drag Reduction in Turbulent Boundary Layers with Half Wave Wall Oscillations
author_sort Mishra, Maneesh
title Drag Reduction in Turbulent Boundary Layers with Half Wave Wall Oscillations
title_short Drag Reduction in Turbulent Boundary Layers with Half Wave Wall Oscillations
title_full Drag Reduction in Turbulent Boundary Layers with Half Wave Wall Oscillations
title_fullStr Drag Reduction in Turbulent Boundary Layers with Half Wave Wall Oscillations
title_full_unstemmed Drag Reduction in Turbulent Boundary Layers with Half Wave Wall Oscillations
title_sort drag reduction in turbulent boundary layers with half wave wall oscillations
publishDate 2015
url https://hdl.handle.net/10356/104296
http://hdl.handle.net/10220/38819
_version_ 1759856787224264704