| Issue |
MATEC Web Conf.
Volume 198, 2018
2018 Asia Conference on Mechanical Engineering and Aerospace Engineering (MEAE 2018)
|
|
|---|---|---|
| Article Number | 03001 | |
| Number of page(s) | 6 | |
| Section | Fluid Mechanics and Modeling | |
| DOI | https://doi.org/10.1051/matecconf/201819803001 | |
| Published online | 12 September 2018 | |
Simulation of flow field in steam ejector and analysis of shock wave characteristics
Shanghai Aircraft Design and Research Institute, Commercial Aircraft Corporation of China Ltd, 5188 Jinke Road, Shanghai, China
Fluent software is used to simulate the two-dimensional flow field in the steam ejector. The generation, development and end of shock in the flow field are analyzed. The influence of the shock wave characteristics on the ejector performance is discussed. The results show that the working back pressure in the steam ejector and the throat diameter of the nozzle all affect the position and intensity of the shock wave. When the shock wave ends prematurely or belatedly , it all affect the performance of the injector.
© The Authors, published by EDP Sciences, 2018
This is an open access article distributed under the terms of the Creative Commons Attribution License 4.0 (http://creativecommons.org/licenses/by/4.0), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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