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http://dx.doi.org/10.5139/JKSAS.2006.34.6.051

Effect of Injection Angle and Length to Diameter Ratios on Drop and Penetration Characteristics in Cross-flow  

Lee, Bong-Soo (한국항공대학교 대학원 항공우주 및 기계공학과)
Ko, Jung-Bin (한국항공대학교 대학원 항공우주 및 기계공학과)
Cho, Woo-Jin (한국항공대학교 대학원 항공우주 및 기계공학과)
Koo, Ja-Ye (한국항공대학교 항공우주 및 기계공학부)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.34, no.6, 2006 , pp. 51-58 More about this Journal
Abstract
The spray characteristics of liquid jet injected into subsonic cross-flow were investigated experimentally. Spray trajectories were captured using CCD camera. Droplet sizes were measured using PDPA and Image Express. The nozzle diameter was 0.5 mm, and its length-to-diameter ratios (L/D) ran$4.11{\times}10^6$ged from 1.0 to 6.0. Experimental results indicate that the breakup point is delayed by increasing gas momentum ratio and the penetration length is decreased by increasing Weber number. At low injection angle(${\theta}$ < $90^{\circ}$), Weber number is dominant parameter for trajectories, but at high injection angle(${\theta}$ > $90^{\circ}$), L/D is dominant parameter for trajectories rather than Weber number.
Keywords
Liquid column; Breakup point; Cross-flow; Momentum ratio; Weber number; Penetration length;
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  • Reference
1 Media Cybernetics corporation. 'The Imaging Experts Technical manual', 1999
2 Fuller, R. P., Wu, P. K., Kirkendall, K. A., and Najad, A. S., 'Effects of injection Angle on Column Breakup Processes of Liquid Jets in Subsonic Cross-flows', AIAA paper 97-2966, July 1997
3 Kihm, K. D., Lyn, G. M., and Son, S. Y., 'Atomization of Cross-Injecting Sprays into Convective Air Stream, Atomization and Sprays', Vol. 5, No. 4, pp. 417-433, 1995   DOI
4 Oda, T., Hiroyasu, H., Arai, M., and Nishida, K., 'Characterization of Liquid Jet Atomization Across a High-Speed Air Stream', JSME International Journal, Series B, Vol. 37, No. 4, pp. 937-944, 1994   DOI   ScienceOn
5 Nguyen, T. T., and Karagozian, A. R., 'Liquid Fuel Jet in Subsonic Cross-flow', Journal of Propulsion and Power, Vol. 8, No. 8, pp. 21-29, 1992   DOI
6 Wotel, G, J., Gallagher, K. E., Caron, S. D., Rosfjord, T. J., Hautman, D. J., and Spadaccini, L.J., 'High Speed Turboramjet Combustor Technology Program', Wright Lab., TR-91-2043, Wright Patterson AFB, OH, 1991
7 Inamura, T, and Nagai, N., 'Spray Characteristics of Liquid Jet Traversing Subsonic Air stream', Journal of Propulsion and Power, Vol. 10, No. 6, pp. 798-803, 1994   DOI   ScienceOn
8 Seay. J., McDnell, V., and Samuelsen, G., 'Atomization and Dispersion from a Radial Airblast Injector in a Subsonic Crossflow', AIAA paper 95-3001, July 1995
9 Wu, P. K., Kirkendall, K. A., Fuller, R. P., and Nejad, A. S., 'Breakup Processes of Liquid Jets in Subsonic Cross-flows', Journal of Propulsion and power, Vol. 13, No. 1, pp. 64-73, 1997   DOI   ScienceOn