A Study on Converging Thin Annular Jets

Author:

Sivakumar D.1,Raghunandan B. N.1

Affiliation:

1. Department of Aerospace Engineering, Indian Institute of Science, Bangalore, 560012, India

Abstract

An interesting feature of jets from liquid-liquid coaxial swirl atomizers used in bipropellant rockets or elsewhere is that the outer jet results in a tulip shaped liquid bulb even at operating pressure levels. In this context, experiments have been performed to study the discharge and tulip characteristics of annular jets through qualitative simulation of outer jet flow conditions at which tulip bulb prevails. It is shown that the discharge coefficient increases steeply with Reynolds number, a trend which is distinct from that of circular orifices. The range of flow conditions at which tulip bulb prevails decreases with the annular gap. If a swirl component is introduced into the annular jet, it alters the discharge characteristics and the tulip range with a tendency to form multiple tulips. Variation of tulip length for different annular gaps shows a common trend when plotted against liquid flow rate. The experimental data of tulip length agree reasonably with the theoretical model reported in literature.

Publisher

ASME International

Subject

Mechanical Engineering

Reference21 articles.

1. Amagai, K., and Arai, M., 1994, “Disintegration Process of a Liquid Jet Injected from a Coaxial Dual Nozzle,” ICLASS-94, July, pp. 71–78.

2. Baird M. H. I. , and DavidsonJ. F., 1962, “Annular Jets-I (Fluid Dynamics),” Chemical Engineering Science, Vol. 17, pp. 467–472.

3. Beer, J. M., and Chigier, N., 1983, Combustion Aerodynamics, Robert E. Krieger Publishing Company.

4. Binnie A. H. , and SquireH. B., 1941, “Liquid Jets of Annular Cross-Section,” The Engineer, Vol. 171, London, pp. 236–238.

5. Boussinesq J. , 1869, “Theorie des experiences de Savart sur la frome que prend une veine liquide apres s’etre choquee contre un plan circulaire,” Comptes Rendus de l’Academie des Sciences, Vol. 69, pp. 128–131.

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