This paper presents the results of an experimental investigation of liquid jet breakup in a cross flow of air under the influence of swirl (swirl numbers 0 and 0.2) at a fixed air flow Mach number 0.12 (typical gas turbine conditions). The experiments have been conducted for various liquid to air momentum flux ratios (q) in the range of 1 to 25. High speed (@ 500 fps) images of the jet breakup process are captured and those images are processed using matlab to obtain the variation of breakup length and penetration height with momentum flux ratio. Using the high speed images, an attempt has been made to understand the physics of the jet breakup process by identification of breakup modes—bag breakup, column breakup, shear breakup, and surface breakup. The results show unique breakup and penetration behavior which departs from the continuous correlations typically used. Furthermore, the images show a substantial spatial fluctuation of the emerging jet resulting in a wavy nature related to effects of instability waves. The results with 15 deg swirl show reduced breakup length and penetration related to the nonuniform distribution of velocity that offers enhanced fuel atomization in swirling fuel nozzles.
Experimental Investigation of Liquid Jet Breakup in a Cross Flow of a Swirling Air Stream
Contributed by the Combustion and Fuels Committee of ASME for publication in the JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Manuscript received November 7, 2013; final manuscript received December 10, 2013; published online January 24, 2014. Editor: David Wisler.
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Sikroria, T., Kushari, A., Syed, S., and Lovett, J. A. (January 24, 2014). "Experimental Investigation of Liquid Jet Breakup in a Cross Flow of a Swirling Air Stream." ASME. J. Eng. Gas Turbines Power. June 2014; 136(6): 061501. https://doi.org/10.1115/1.4026244
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