Abstract
To reveal the internal flow characteristics of a compressor cascade before and after separation control by internal vortex generator jets (VJTs), the change in the separate configuration of a high subsonic compressor cascade before and after the control was analyzed in detail according to a topology theory, and the topological and vortex structure models were given. Moreover, loss characteristics were also considered. The calculation results show that the end-wall jet vortex generator changed the separate configuration of the flow fields, which effectively delayed the suction surface flow separation. After using flow control, the number of odd-points was significantly reduced, and the end-wall cross flow was effectively controlled. Furthermore, the passage vortex and concentrated shedding vortex were weakened, and the trailing edge shedding vortex at mid-span basically disappeared. The end-wall boundary layer loss and profile loss were not obvious, while the secondary flow loss is up to 38%. The end-wall VGJs have a weak influence on the middle of the cascade. Therefore, it is necessary to adopt a combined flow control to further improve the flow field structure.
| Translated title of the contribution | Effect of end-wall vortex generator jets on the separate structure in high subsonic compressor cascade |
|---|---|
| Original language | Chinese (Traditional) |
| Pages (from-to) | 1314-1320 |
| Number of pages | 7 |
| Journal | Harbin Gongcheng Daxue Xuebao/Journal of Harbin Engineering University |
| Volume | 39 |
| Issue number | 8 |
| DOIs | |
| State | Published - 5 Aug 2018 |
| Externally published | Yes |
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