Experimental investigations of the effect of Reynolds number on a plane jet

Deo, Ravinesh C. and Mi, Jianchun and Nathan, Graham J. (2007) Experimental investigations of the effect of Reynolds number on a plane jet. In: 16th Australasian Fluid Mechanics Conference (AFMC 2007), 3-7 Dec 2007, Gold Coast, Queensland.

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The effect of Reynolds number, Re = Uo,cH/μ , where Uo,c is
the nozzle exit centreline velocity, H is the slot-opening width and n is the kinematic viscosity of air) on the velocity field of a turbulent plane jet from a radially contoured nozzle of aspect ratio 60 is investigated. Measurements are conducted using a single wire anemometer over an axial distance of 160h. The Reynolds number is varied between 1,500 and 16,500. Results show that the Re affects various flow properties such as the velocity decay rate, half-width and turbulence intensity. The significant dependence on Re of the mean flow field persists till Re = 16,500, while the Re effect on the turbulent properties
becomes weaker above Re = 10,000. The present investigation
also suggests that an increase in Re leads to a higher rate of mixing in the near field but a lower rate in the far field.

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Item Type: Conference or Workshop Item (Commonwealth Reporting Category E) (Paper)
Refereed: Yes
Item Status: Live Archive
Additional Information: No evidence of copyright restrictions.
Faculty / Department / School: Historic - Faculty of Sciences - Department of Maths and Computing
Date Deposited: 14 May 2010 06:36
Last Modified: 14 Jun 2016 01:25
Uncontrolled Keywords: plane jet, Reynolds number effect
Fields of Research : 09 Engineering > 0915 Interdisciplinary Engineering > 091508 Turbulent Flows
09 Engineering > 0915 Interdisciplinary Engineering > 091504 Fluidisation and Fluid Mechanics
Socio-Economic Objective: E Expanding Knowledge > 97 Expanding Knowledge > 970109 Expanding Knowledge in Engineering
URI: http://eprints.usq.edu.au/id/eprint/7420

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