Drag Reduction of a Turbulent Boundary Layer over an Oscillating Wall and Its Variation with Reynolds Number

Joint Authors

Skote, Martin
Mishra, Maneesh
Wu, Yanhua

Source

International Journal of Aerospace Engineering

Issue

Vol. 2015, Issue 2015 (31 Dec. 2015), pp.1-9, 9 p.

Publisher

Hindawi Publishing Corporation

Publication Date

2015-12-14

Country of Publication

Egypt

No. of Pages

9

Abstract EN

Spanwise oscillation applied on the wall under a spatially developing turbulent boundary layer flow is investigated using direct numerical simulation.

The temporal wall forcing produces a considerable drag reduction over the region where oscillation occurs.

Downstream development of drag reduction is investigated from Reynolds number dependency perspective.

An alternative to the previously suggested power-law relation between Reynolds number and peak drag reduction values, which is valid for channel flow as well, is proposed.

Considerable deviation in the variation of drag reduction with Reynolds number between different previous investigations of channel flow is found.

The shift in velocity profile, which has been used in the past for explaining the diminishing drag reduction at higher Reynolds number for riblets, is investigated.

A new predictive formula is derived, replacing the ones found in the literature.

Furthermore, unlike for the case of riblets, the shift is varying downstream in the case of wall oscillations, which is a manifestation of the fact that the boundary layer has not reached a new equilibrium over the limited downstream distance in the simulations.

Taking this into account, the predictive model agrees well with DNS data.

On the other hand, the growth of the boundary layer does not influence the drag reduction prediction.

American Psychological Association (APA)

Skote, Martin& Mishra, Maneesh& Wu, Yanhua. 2015. Drag Reduction of a Turbulent Boundary Layer over an Oscillating Wall and Its Variation with Reynolds Number. International Journal of Aerospace Engineering،Vol. 2015, no. 2015, pp.1-9.
https://search.emarefa.net/detail/BIM-1064550

Modern Language Association (MLA)

Skote, Martin…[et al.]. Drag Reduction of a Turbulent Boundary Layer over an Oscillating Wall and Its Variation with Reynolds Number. International Journal of Aerospace Engineering No. 2015 (2015), pp.1-9.
https://search.emarefa.net/detail/BIM-1064550

American Medical Association (AMA)

Skote, Martin& Mishra, Maneesh& Wu, Yanhua. Drag Reduction of a Turbulent Boundary Layer over an Oscillating Wall and Its Variation with Reynolds Number. International Journal of Aerospace Engineering. 2015. Vol. 2015, no. 2015, pp.1-9.
https://search.emarefa.net/detail/BIM-1064550

Data Type

Journal Articles

Language

English

Notes

Includes bibliographical references

Record ID

BIM-1064550