The spray cone angles produced by several simplex pressure-swirl nozzles are examined using three liquids whose viscosities range from 0.001 to 0.012 kg/ms (1 to 12 cp). Measurements of both the visible spray cone angle and the effective spray cone angle are carried out over wide ranges of injection pressure and for five different values of the discharge orifice length/diameter ratio. The influence of the number of swirl chamber feed slots on spray cone angle is also examined. The results show that the spray cone angle widens with increase in injection pressure but is reduced by increases in liquid viscosity and/or discharge orifice length/diameter ratio. Variation in the number of swirl chamber feed slots between one and three has little effect on the effective spray cone angle.
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January 1992
Research Papers
Factors Influencing the Effective Spray Cone Angle of Pressure-Swirl Atomizers
S. K. Chen,
S. K. Chen
Thermal Science and Propulsion Center, Purdue University, West Lafayette, IN 47907
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A. H. Lefebvre,
A. H. Lefebvre
Thermal Science and Propulsion Center, Purdue University, West Lafayette, IN 47907
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J. Rollbuhler
J. Rollbuhler
NASA-Lewis Research Center, Cleveland, OH 44135
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S. K. Chen
Thermal Science and Propulsion Center, Purdue University, West Lafayette, IN 47907
A. H. Lefebvre
Thermal Science and Propulsion Center, Purdue University, West Lafayette, IN 47907
J. Rollbuhler
NASA-Lewis Research Center, Cleveland, OH 44135
J. Eng. Gas Turbines Power. Jan 1992, 114(1): 97-103 (7 pages)
Published Online: January 1, 1992
Article history
Received:
December 1, 1990
Online:
April 24, 2008
Citation
Chen, S. K., Lefebvre, A. H., and Rollbuhler, J. (January 1, 1992). "Factors Influencing the Effective Spray Cone Angle of Pressure-Swirl Atomizers." ASME. J. Eng. Gas Turbines Power. January 1992; 114(1): 97–103. https://doi.org/10.1115/1.2906313
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