Effectiveness of secondary tabs for supersonic mixing |
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Authors: | S Hari J Kurian |
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Institution: | (1) Department of Aerospace Engineering Indian Institute of Technology, Madras 600036, India e-mail: kurian@aero.iitm.ernet.in, IN |
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Abstract: | The effect of vortex generators, in the form of small tabs projecting into the flow at the nozzle exit, aided by secondary
tabs on either side, on the mixing characteristics of an axisymmetric jet at Mach number 1.7 is investigated. Experimental
studies on the basic features of the jet from a nozzle with secondary tabs are conducted to assess the free jet characteristics
as well as the momentum and thermal mixing behavior. The secondary tabs were found to increase the jet spread and distort
the jet cross-section and were found to cause substantial enhancement of mixing of supersonic jets. Jet structure is observed
using flow-visualization techniques. LLS images are employed to obtain cross-sectional views of the jet with the introduction
of secondary tabs. The ability of secondary tabs to eliminate the screech noise of the supersonic jet is also observed.
Received: 3 February 2000/Accepted: 8 February 2001 |
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