Technical Papers
Mar 21, 2017

Conditioned Analysis of Effervescent Atomization

Publication: Journal of Energy Engineering
Volume 143, Issue 5

Abstract

Effervescent atomizers have a number of significant advantages over conventional injectors. They can operate at much lower injection pressures, their atomization performance is largely insensitive to fuel physical properties, and very fine atomization can be achieved at lower air flow-rates when compared to air-blast atomizers. Despite these advantages, there is a lack of quantitative data describing the near-field atomization zone, which is difficult to probe due to the unstable nature of effervescent fragmentation. This lack of data has prevented a fundamental understanding of this atomization mode and delayed the development of advanced numerical models. Here, the near-field characteristics of a series of effervescent sprays are examined using advanced image processing. The study provides new quantitative insights into the nature of the regime transitions that occur as a function of the gas-to-liquid ratio (GLR). The distinct regime transitions, noted through quantitative measurements of the liquid jet outer diameter, closely coincide with previously quoted bubble type and transitional tree-regime transitions. The distribution of the outer diameter of the ejected air-laden liquid jet progresses from bimodal at low GLR values (<0.5%) to monomodal distribution at a higher GLR. Measurements of ligament thickness in the near field have allowed for direct evaluation of a previously developed analytical model that predicts droplet Sauter mean diameter (SMD) as a function of the GLR. This model has been confirmed here over a wider GLR range by using number-based conditioning and further extended into a simple analytical model that can estimate the total number of objects generated per unit time.

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Acknowledgments

The work was funded by the Australian Research Council.

References

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Published In

Go to Journal of Energy Engineering
Journal of Energy Engineering
Volume 143Issue 5October 2017

History

Received: Sep 16, 2016
Accepted: Dec 19, 2016
Published ahead of print: Mar 21, 2017
Published online: Mar 22, 2017
Discussion open until: Aug 22, 2017
Published in print: Oct 1, 2017

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Authors

Affiliations

A. Kourmatzis, Ph.D. [email protected]
Dept. of Engineering, Macquarie Univ., NSW 2109, Australia (corresponding author). E-mail: [email protected]
Aerospace, Mechanical and Mechatronic Engineering, Univ. of Sydney, NSW 2006, Australia. E-mail: [email protected]
A. R. Masri, Ph.D. [email protected]
Professor, Aerospace, Mechanical and Mechatronic Engineering, Univ. of Sydney, NSW 2006, Australia. E-mail: [email protected]

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