年間 4 号発行
ISSN 印刷: 1065-3090
ISSN オンライン: 1940-4336
Indexed in
VISUALIZATION OF SUPERSONIC LIQUID FUEL JETS
要約
Results from further studies on supersonic liquid fuel jets injected into ambient air conditions are reported in this paper. In the study, a special technique, the projectile impact driven method, is used to generate supersonic liquid fuel jets. A high-speed video camera and a shadowgraph optical system are employed to obtain visualizations. Effects of fuel properties and nozzle geometries on the characteristics, tip velocity, and penetration distance of the jets are the main focus. Strong multiple high-frequency jet pulses generated within the duration of a single shot impact are usually found in the conical nozzle but are less obvious in the nonconical nozzle. These associated multiple jet shock waves have been clearly captured in the visualization. In addition, the preliminary study on the numerical simulation of supersonic liquid (water) jets using AUTODYN-2DTM code is presented. Some characteristics such as jet tip velocity, jet shock wave angle, and pulsing behavior can be predicted. Overall, at this stage, the results show good promise for further development of this type of simulation.
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