posted on 2018-11-14, 09:31authored byMuhammad A. Kamran
The field of jet mixing enhancement has interested researchers for a long time because of its practical
significance in many engineering areas: combustion, noise reduction, IR signature reduction. In the
military aircraft context, the largest sources of IR radiation are the engine afterburner, propulsion
nozzle, and jet exhaust plume, where gas and metal temperatures are highest. Rapid mixing of the jet
plume with the ambient air offers a number of interesting possibilities for IR reduction, including noise
reduction as an added benefit. Many techniques to achieve enhanced jet mixing have been proposed; all
have limitations and no technique has been clearly proven to be optimum. An active control technique
which has shown promise is the use of control jets - a discrete number of small radially penetrating jets
introduced around the primary jet periphery at nozzle exit. The control jets may be steady or pulsed.
However, the literature to date largely covers studies on control jet effectiveness at low Reynolds
numbers and mostly under low Mach number, essentially incompressible, conditions - far removed
from the regime of practical application. The fact that control jets can be designed according to
requirements, and in particular can be turned off when not required, argues that this technique is worthy
of further investigation, but with a specific emphasis on high Re, high Mach number compressible jet
flows. This is the focus of the current study, which constituted both experimental and computational
investigations. [Continues.]
Funding
North-West Frontier Province University of Engineering and Technology (Peshawar, Pakistan).
History
School
Aeronautical, Automotive, Chemical and Materials Engineering
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Publication date
2009
Notes
A Doctoral Thesis. Submitted in partial fulfilment of the requirements for the award of the degree of Doctor of Philosophy at Loughborough University.