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Perforated Arc-Tabs for Jet Control

  • Dharmahinder Singh Chand EMAIL logo , S. Thanigaiarasu , S. Elangovan und E. Rathakrishnan
Veröffentlicht/Copyright: 14. Juni 2011
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International Journal of Turbo & Jet-Engines
Aus der Zeitschrift Band 28 Heft 2

Abstract

This paper presents the effectiveness of perforated arc tabs to enhance the mixing of axi-symmetric subsonic and sonic jets. Measurements of centerline velocity decay and velocity distribution in the directions along and normal to the tabs were carried out in the controlled jet, from a convergent nozzle with two arc-tabs placed at diametrically opposite locations at the nozzle exit, were carried out. Similar measurements were done for the uncontrolled jets, for comparison. Mach 0.6, 0.7, 0.9 and sonic jet at nozzle pressure ratios 2 and 3 were tested. It is found that the perforated arc-tabs greatly enhance the jet mixing of both subsonic and sonic jets. The core length comes down by 65%, 66%, 62% and 75%, for Mach 0.6, 0.7, 0.9 and correctly expanded Mach 1 jets, respectively.


Corresponding author: Dharmahinder Singh Chand, Department of Aerospace Engineering, Madras Institute of Technology, Anna University, Chennai-44, India

Received: 2011-01-25
Revised: 2011-02-20
Accepted: 2011-03-03
Published Online: 2011-06-14
Published in Print: 2011-June

Copyright © 2011 De Gruyter

Heruntergeladen am 1.11.2025 von https://www.degruyterbrill.com/document/doi/10.1515/tjj.2011.012/pdf
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