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

المؤلفون المشاركون

Skote, Martin
Mishra, Maneesh
Wu, Yanhua

المصدر

International Journal of Aerospace Engineering

العدد

المجلد 2015، العدد 2015 (31 ديسمبر/كانون الأول 2015)، ص ص. 1-9، 9ص.

الناشر

Hindawi Publishing Corporation

تاريخ النشر

2015-12-14

دولة النشر

مصر

عدد الصفحات

9

الملخص 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.

نمط استشهاد جمعية علماء النفس الأمريكية (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

نمط استشهاد الجمعية الأمريكية للغات الحديثة (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

نمط استشهاد الجمعية الطبية الأمريكية (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

نوع البيانات

مقالات

لغة النص

الإنجليزية

الملاحظات

Includes bibliographical references

رقم السجل

BIM-1064550