Volume 12, Issue 1 pp. 575-576
Section 13
Free Access

Variation of friction drag via spanwise transversal surface waves

Pascal Meysonnat

Corresponding Author

Pascal Meysonnat

Institue of Aerodyamics, RWTH Aachen University, 52062 Aachen, Germany

phone +49 241 80 90396, fax +49 241 80 92257Search for more papers by this author
Stephan Klumpp

Stephan Klumpp

Institue of Aerodyamics, RWTH Aachen University, 52062 Aachen, Germany

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Matthias Meinke

Matthias Meinke

Institue of Aerodyamics, RWTH Aachen University, 52062 Aachen, Germany

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Wolfgang Schröder

Wolfgang Schröder

Institue of Aerodyamics, RWTH Aachen University, 52062 Aachen, Germany

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First published: 03 December 2012
Citations: 2

Abstract

Introducing spanwise velocity components into the near-wall flow field of a turbulent boundary layer has shown to be an effective mean of influencing the wall shear stress. The underlying physical mechanisms leading to the drag reduction have however not been fully understood. The presented investigation uses sinusoidal transversal travelling surface waves to influence the near-wall turbulence to achieve drag reduction. Two distinct wave configurations are analysed in detail and compared to an unactuated turbulent flat plate boundary layer flow to gain inside into the drag reducing mechanisms. (© 2012 Wiley-VCH Verlag GmbH & Co. KGaA, Weinheim)

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