Abstract Investigation of liquid breakup mechanism is an important role to improve performance of solid rocket motor (SRM) to reduce the erosion damage near nozzle a throat section. Protection of the nozzle wall could be achieved by enhancing liquid breakup mechanism of the liquid alumina inside combustion chamber before bulk alumina slug erodes the nozzle section. This paper presents a study of air and water two-phase straight channel experiment that simulates the breakup mechanism of alumina. The study of liquid breakup mechanism is carried out by analyzing high-speed camera image through image processing technic during this straight channel two-phase experiment. This image processing extract the particle size and counts data from each frame of high-speed pictures, therefore, we have mass accumulation distribution from different particle size and his information could be useful information for combustion channel design.
Study of Liquid Breakup Mechanism Through a High-Speed Gas Flow
Proceedings of the 5th International Conference on Jets, Wakes and Separated Flows (ICJWSF2015) ; 8 ; 467-474
Springer Proceedings in Physics ; 185 , 8
2016-01-01
8 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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