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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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 |
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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. |
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School of Mechanical and Aerospace Engineering |
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School of Mechanical and Aerospace Engineering Mishra, Maneesh Skote, Martin |
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Mishra, Maneesh Skote, Martin |
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Mishra, Maneesh Skote, Martin Drag Reduction in Turbulent Boundary Layers with Half Wave Wall Oscillations |
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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 |
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Drag Reduction in Turbulent Boundary Layers with Half Wave Wall Oscillations |
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Drag Reduction in Turbulent Boundary Layers with Half Wave Wall Oscillations |
title_sort |
drag reduction in turbulent boundary layers with half wave wall oscillations |
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2015 |
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https://hdl.handle.net/10356/104296 http://hdl.handle.net/10220/38819 |
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