摘要
Combustion instability is a very important issue in the development of the propulsion systems used in aerospace. It is very important to associate the high frequency combustion instabilities with the acoustic characteristics of the combustion chamber. In this paper, the effects of various baffle injectors which were installed on the injector faceplate on the first-order tangential acoustic mode were investigated theoretically and experimentally. The effects of the gap between adjacent injectors on the first-order tangential acoustic mode in a cylindrical chamber were considered. The acoustic admittance of the injectors was derived. The results showed that the amplitude and frequency of the first-order tangential acoustic mode increase with the increase in the gap between adjacent injectors, but decrease with the increase in the number and height of the baffles.The baffle injectors have a greater influence on the amplitude and frequency of the first-order tangential acoustic mode than the baffle blades.
基金
the National Natural Science Foundation of China (Nos. 51806057, 52005152 and 12042211)
the Natural Science Foundation of Hebei, China (Nos. E2019202460 and E2019202451)
Tianjin Science and Technology Project, China (No. 19YFZCSF00850)
the Key Research Program Projects of Hebei Province, China (No. 19274502D)
the Industrial Technology Research of Hebei University of Technology, China (No. ZBYJY201902)
