This paper describes an experimental investigation of the effects of air-assist upon the penetration and dispersion of a liquid fuel jet that is injected into cross-flowing air. The spray patterns across the central longitudinal plane were investigated at flow conditions similar to those encountered at the combustor inlet of a modern gas turbine engine. Temperatures of the cross-flow and assist air were at 316 and 427°C, while test-channel pressures were set at 2.02 and 2.53MPa. Jet-A fuel was injected through a wall-recessed plain orifice into a rectangular test-channel where the cross-flow air velocity was Ucross-flow=75m/s. Assist air was injected from four slots surrounding the fuel orifice within the wall-recessed well. The air-assist jets impinged upon the fuel jet at a 45° angle. Pressure drops across the air-slots were limited to ≤4% of test-channel pressure to simulate the difference between stagnation and static pressures on a typical fuel-air mixer/injector. Thus, the assist-air-to-liquid fuel mass-flow ratios (ALR) were limited to 0.41, which was much lower than those used in traditional airblast atomizers with ALR in the range of 1 to 10. Momentum-flux ratios (J) of the fuel jet to cross-flow were varied between J=5 to 40. A 355nm planar laser was used to illuminate the spray’s central plane to capture images of liquid droplets Mie-scattering. An attempt was made at correlating the trajectories of the jet using an effective momentum-flux ratio Jeff that accounts for air-assist jets’ momentum. It was discovered that air-assist had limited influence on the spray’s outer-edge penetration, while it strongly enhances the penetration of the inner-edge and spray centerline. Air-assist’s effects were also found to be proportional to ALR. Contrary to the results of airblast jet-in-cross-flow researches, it was found that at J∼5, when the sprays’ inner-edges were close to the wall, air-assist enhanced the inner-edge penetration in a manner that was not well-captured by Jeff. Finally, it was also observed that sprays at 2.53MPa were more sensitive to J and air-assist variations than sprays at 2.02MPa.
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ASME Turbo Expo 2015: Turbine Technical Conference and Exposition
June 15–19, 2015
Montreal, Quebec, Canada
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-5668-0
PROCEEDINGS PAPER
Effect of Air-Assist on Liquid Jet Penetration and Dispersion in a Cross-Flow of Hot, High-Pressure Air Available to Purchase
Zu Puayen Tan,
Zu Puayen Tan
Georgia Institute of Technology, Atlanta, GA
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Eugene Lubarsky,
Eugene Lubarsky
Georgia Institute of Technology, Atlanta, GA
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Oleksandr Bibik,
Oleksandr Bibik
Georgia Institute of Technology, Atlanta, GA
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Dmitriy Shcherbik,
Dmitriy Shcherbik
Georgia Institute of Technology, Atlanta, GA
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Ben T. Zinn
Ben T. Zinn
Georgia Institute of Technology, Atlanta, GA
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Zu Puayen Tan
Georgia Institute of Technology, Atlanta, GA
Eugene Lubarsky
Georgia Institute of Technology, Atlanta, GA
Oleksandr Bibik
Georgia Institute of Technology, Atlanta, GA
Dmitriy Shcherbik
Georgia Institute of Technology, Atlanta, GA
Ben T. Zinn
Georgia Institute of Technology, Atlanta, GA
Paper No:
GT2015-42239, V04AT04A024; 10 pages
Published Online:
August 12, 2015
Citation
Tan, ZP, Lubarsky, E, Bibik, O, Shcherbik, D, & Zinn, BT. "Effect of Air-Assist on Liquid Jet Penetration and Dispersion in a Cross-Flow of Hot, High-Pressure Air." Proceedings of the ASME Turbo Expo 2015: Turbine Technical Conference and Exposition. Volume 4A: Combustion, Fuels and Emissions. Montreal, Quebec, Canada. June 15–19, 2015. V04AT04A024. ASME. https://doi.org/10.1115/GT2015-42239
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