Research output per year
Research output per year
J. P. Gostelow*, R. L. Thomas, D. S. Adebayo
Research output: Chapter in Book/Published conference output › Conference publication
Further evidence on the similarities between transition and separation phenomena occurring in turbomachinery and wind tunnel flows is provided by measurements on a large scale flat plate under a strong adverse pressure gradient. The flat plate has a long laminar separation bubble and is subjected to a range of disturbances with triggering caused by injection of a transverse jet and subsequently by wakes generated by rods moving transversely upstream of the leading edge. Wakes were originally presented individually. Each individual wake provoked a vigorous turbulent patch, resulting in the instantaneous collapse of the separation bubble. This was followed by a very strong, and stable, calmed region. Following the lead given by the experiments of Gutmark and Blackwelder on triggered turbulent spots, wakes were then presented in pairs at different wake spacing intervals. In this way wake interaction effects could be investigated in more detail. As in the work on triggered turbulent spots the spacing between impinging wakes was systematically varied; it was found that for close wake spacings the calmed region acted to suppress the turbulence in the following turbulent patch. To investigate whether this phenomenon was a recurring one, or whether the flow then reverted back to its unperturbed state, the experiments were repeated with three and four rods instead of two. This has the potential for making available a wide range of variables including direction and speed of rod rotation. It was found that the subsequent wakes were also suppressed by the calming effect. It may be anticipated that this repeating situation is present in a turbomachine, resulting in hidden benefits for blade count and efficiency. There may also conceivably be blade loading advantages whilst retaining favorable heat transfer conditions in high pressure turbines or stall margin in axial compressors. The inherent and prospective benefits of the calming effect therefore need to be understood thoroughly and new opportunities exploited where this is feasible.
| Original language | English |
|---|---|
| Title of host publication | Proceedings of the ASME Turbo Expo 2007 - Power for Land, Sea, and Air |
| Publisher | American Society of Mechanical Engineers(ASME) |
| Pages | 1105-1113 |
| Number of pages | 9 |
| ISBN (Print) | 079184790X, 9780791847909 |
| DOIs | |
| Publication status | Published - 10 Mar 2019 |
| Event | 2007 ASME Turbo Expo - Montreal, Que., Canada Duration: 14 May 2007 → 17 May 2007 |
| Name | Proceedings of the ASME Turbo Expo |
|---|---|
| Volume | 4 PART B |
| Conference | 2007 ASME Turbo Expo |
|---|---|
| Country/Territory | Canada |
| City | Montreal, Que. |
| Period | 14/05/07 → 17/05/07 |
Research output: Contribution to journal › Article › peer-review