Effect of steady rotation on low Reynolds number vortex shedding behind a circular cylinder


Autoria(s): Ramesh, ON; Patwardhan, Saurabh S
Data(s)

01/08/2013

Resumo

In this paper control of oblique vortex shedding in the wake behind a straight circular cylinder is explored experimentally and computationally. Towards this, steady rotation of the cylinder about its axis is used as a control device. Some limited studies are also performed with a stepped circular cylinder, where at the step the flow is inevitably three-dimensional irrespective of the rotation rate. When there is no rotation, the vortex shedding pattern is three dimensional as described in many previous studies. With a non-zero rotation rate, it is demonstrated experimentally as well as numerically that the shedding pattern becomes more and more two-dimensional. At sufficiently high rotation rates, the vortex shedding is completely suppressed.

Formato

application/pdf

Identificador

http://eprints.iisc.ernet.in/47548/1/Jou_Flui_Stru_41_175_2013.pdf

Ramesh, ON and Patwardhan, Saurabh S (2013) Effect of steady rotation on low Reynolds number vortex shedding behind a circular cylinder. In: Journal of Fluids and Structures, 41 . pp. 175-186.

Publicador

Elsevier Science

Relação

http://dx.doi.org/10.1016/j.jfluidstructs.2013.05.007

http://eprints.iisc.ernet.in/47548/

Palavras-Chave #Aerospace Engineering (Formerly, Aeronautical Engineering)
Tipo

Journal Article

PeerReviewed