Perforated Rib in Turbulent Boundary Layer

Author:

Afanasiev Valery N.1,Kong Dehai1,Isaev S. A.2

Affiliation:

1. Department of Thermophysics, Bauman Moscow State Technical University, 2nd Baumanskaya Street, 5, Moscow 105005, Russia

2. Department of Mechanics, Saint-Petersburg State University of Civil Aviation, Pilots's Street, 38, Saint-Petersburg 196210, Russia

Abstract

Abstract This study presents the results of the experimental study on hydrodynamics and heat transfer in separation zone in front and behind a single rectangular perforated rib mounted on a flat plate. The effects of perforation open-area ratio (β = 12%, 23.5%, and 44%) and the location of the hole on the rib (at the bottom, at the top, and in a staggered arrangement) on the mean and fluctuating characteristics of the turbulent dynamic and thermal boundary layers in the median section of the plate were examined. It was established that the stagnant and recirculation zones in the front and behind the perforated rib were shifted and became smaller or disappeared.

Publisher

ASME International

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science

Reference15 articles.

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2. On the Improvement of the Poor Heat Transfer Lee-Side Regions of Square Cross-Section Ribbed Channels;Numer. Heat Transfer: Part A: Appl.,2014

3. Rectangular Ribs in Turbulent Boundary Layer on the Initially Smooth Surface;J. Phys.: Conf. Ser.,2017

4. Turbulent Heat and Fluid Flow in a Passage Dis-Turbed by Detached Perforated Ribs of Different Heights;Int. J. Heat Mass Transfer,1998

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