DESIGN, DEVELOPMENT AND PERFORMANCE EVALUATION OF NEW SWIRL EFFERVESCENT INJECTOR
DOI:
https://doi.org/10.11113/jt.v75.2813Keywords:
Swirl effervescent injector, injector fabrication, spray breakup, shadowgraphAbstract
The swirl effervescent injector has more desirable characteristics because it allows a system to run on low injection pressure and yet is still able to achieve an efficient atomization. In previous studies on other types of injectors, spray breakup length was reported as one of the important spray characteristics since a shorter spray breakup length tend to provide an earlier atomization. However, intensive studies on spray characteristics of the swirl effervescent injector are scarce. This paper is intended to describe the geometrical design procedures and performance assessments of a newly developed swirl effervescent injector. In designing the injector, a similitude technique was deployed to find the best design attributes among 4 existing injectors. The desired attributes were incorporated into the development of the injector. The swirl chamber was made from Perspex to permit visualization of the internal flow. A test rig was built to evaluate the injector’s performance. Water was used as the working fluid and nitrogen gas as the atomizing agent. The spray breakup characteristics were observed at different GLR and recorded using high-speed shadowgraph technique. For the analyses of the video recordings and the conversion into image sequences, ImageJ and specific software have been deployed. It was found that the introduction of the swirl-generating vane prior to the discharge orifice has assisted in shortening the spray breakup length at any amount of GLR. Â
References
Ghaffar, Z. A., A. H. A. Hamid, and M. S. F. M. Rashid. 2012. Spray Characteristics of Swirl Effervescent Injector in Rocket Application: A Review. Applied Mechanics and Materials. 225: 423-428.
Gadgil, H. and B. N. Raghunandan. 2011. Some Features of Spray Breakup in Effervescent Atomizers. Experiments in Fluids. 50: 329-338.
Hamid, A. H. A. and R. Atan. 2009. Spray Characteristics of Jet–swirl Nozzles for Thrust Chamber Injector. Aerospace Science and Technology. 13: 192-196.
Hussein, A., M. Hafiz, H. Rashid, A. Halim, W. Wisnoe, and S. Kasolang. 2012. Characteristics of Hollow Cone Swirl Spray at Various Nozzle Orifice Diameters. Jurnal Teknologi. 58: 1-4.
Jagannathan, T. K., R. Nagarajan, and K. Ramamurthi. 2011. Effect of Ultrasound on Bubble Breakup Within the Mixing Chamber of an Effervescent Atomizer. Chemical Engineering and Processing: Process Intensification. 50: 305-315.
Ow, C. S. 1980. Studies of Two-Phase Turbulent Pipe Flow. PhD Thesis. Mechanical Engineering Department, Imperial College, London.
Ghaffar, Z. A., S. Kasolang, and A. H. A. Hamid. 2014. Characteristics of Swirl Effervescent Atomizer Spray Angle. Applied Mechanics and Materials. 607: 108-111.
Sovani, S. D., P. E. Sojka, and A. H. Lefebvre. 2001. Effervescent Atomization. Progress in Energy and Combustion Science. 27: 483-521.
Jedelsky, J., M. Jicha, J. Slama, and J. Otahal. 2009. Development of an Effervescent Atomizer for Industrial Burners. Energy & Fuels. 23: 6121-6130.
Rahman, M. A., M. Balzan, T. Heidrick, and B. A. Fleck. 2012. Effects of the Gas Phase Molecular Weight and Bubble Size on Effervescent Atomization. International Journal of Multiphase Flow. 38: 35-52.
Lefebvre, A. H. 1988. A Novel Method of Atomization with Potential Gas Turbine Applications. Defense Science Journal. 38: 353-361.
Rashid, M. S. F. M., A. H. A. Hamid, O. C. Sheng, and Z. A. Ghaffar. 2012. An Experimental Investigation on the Effect of Various Swirl Atomizer Orifice Geometries on the Air Core Diameter. Applied Mechanics and Materials. 225: 32-37.
Downloads
Published
Issue
Section
License
Copyright of articles that appear in Jurnal Teknologi belongs exclusively to Penerbit Universiti Teknologi Malaysia (Penerbit UTM Press). This copyright covers the rights to reproduce the article, including reprints, electronic reproductions, or any other reproductions of similar nature.