Numerical analysis of the shock train evolution in planar nozzles with throat length
In the present investigation, the behavior of compressible flow in planar nozzles with throat length is analyzed to determine the flow velocity range and pressure fluctuations in the throat section. The flow field was simulated in 2D computational domains with the ANSYS-Fluent R16.2 code. The RANS m...
| 發表在: | FME Transactions |
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| Main Authors: | , , |
| 格式: | Article |
| 語言: | 英语 |
| 出版: |
University of Belgrade - Faculty of Mechanical Engineering, Belgrade
2023-01-01
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| 主題: | |
| 在線閱讀: | https://scindeks-clanci.ceon.rs/data/pdf/1451-2092/2023/1451-20922304595T.pdf |