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Triangular Tabs for Supersonic Jet Control

Name: Triangular Tabs for Supersonic Jet Control
Brand: Scholars' Press
SKU: 07043873
Price: 31081 HUF
Availability: InStock
Author: Arun Kumar P.
ISBN: 9783639702316

An Experimental Study

Arun Kumar P.

Language

English

Book Paperback

Libristo code: 07043873

Publishers Scholars' Press, November 2013

An experimental investigation has been carried out to study the mixing promoting efficiency of right... Full description

Libristo code: 07043873

212 b

31 081 Ft

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An experimental investigation has been carried out to study the mixing promoting efficiency of right-angled and isosceles triangular tabs with sharp and truncated vertices. The mixing promotion caused by two identical triangular tabs, offering a geometrical blockage of 2.5% each, placed at the exit of a Mach 2 circular nozzle, was studied in the presence of adverse and marginally favourable pressure gradients. The results of the present study demonstrate the validity of the hypothesis that, the triangular tabs shedding vortices of continuously varying sizes is a better mixing promoter than the rectangular tabs, shedding vortices of uniform size. Furthermore, the truncated vertex triangular tab is found to be a better mixing promoter than the sharp vertex triangular tab, at all levels of expansion of the present study.