Details
| Original language | English |
|---|---|
| Title of host publication | Turbomachinery |
| Publisher | American Society of Mechanical Engineers(ASME) |
| Number of pages | 14 |
| ISBN (electronic) | 9780791858585 |
| Publication status | Published - 5 Nov 2019 |
| Event | ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition, GT 2019 - Phoenix, United States Duration: 17 Jun 2019 → 21 Jun 2019 |
Publication series
| Name | Proceedings of the ASME Turbo Expo |
|---|---|
| Volume | 2D-2019 |
Abstract
In this paper, we propose the concept of thermal end-wall contouring (TEWC) as a novel approach to reducing secondary-flow and boundary-layer losses in turbomachines and ducts by means of thermally manipulating the boundary layer. We introduce, for the first time, the general concept of TEWC and provide a proof of concept using the example of a bent duct. The results demonstrate that a considerable impact on the flow field is achieved not only by mean heat flux across the end-wall of the duct, but also by the spatial distribution of the heat fluxes.
ASJC Scopus subject areas
- Engineering(all)
- General Engineering
Cite this
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Turbomachinery. American Society of Mechanical Engineers(ASME), 2019. (Proceedings of the ASME Turbo Expo; Vol. 2D-2019).
Research output: Chapter in book/report/conference proceeding › Conference contribution › Research › peer review
}
TY - GEN
T1 - Thermal end-wall contouring
AU - Mimic, Dajan
AU - Oettinger, Marcel
AU - Jätz, Christoph
AU - Herbst, Florian
AU - Seume, Jörg Reinhart
N1 - Funding information: The authors acknowledge the contribution of the DLR Institute of Propulsion Technology and MTU Aero Engines AG for providing TRACE. The authors thank the Leibniz Universität Hannover IT Services (LUIS) for providing computational resources. The authors would further like to acknowledge Pointwise Inc. for providing academic licenses.
PY - 2019/11/5
Y1 - 2019/11/5
N2 - In this paper, we propose the concept of thermal end-wall contouring (TEWC) as a novel approach to reducing secondary-flow and boundary-layer losses in turbomachines and ducts by means of thermally manipulating the boundary layer. We introduce, for the first time, the general concept of TEWC and provide a proof of concept using the example of a bent duct. The results demonstrate that a considerable impact on the flow field is achieved not only by mean heat flux across the end-wall of the duct, but also by the spatial distribution of the heat fluxes.
AB - In this paper, we propose the concept of thermal end-wall contouring (TEWC) as a novel approach to reducing secondary-flow and boundary-layer losses in turbomachines and ducts by means of thermally manipulating the boundary layer. We introduce, for the first time, the general concept of TEWC and provide a proof of concept using the example of a bent duct. The results demonstrate that a considerable impact on the flow field is achieved not only by mean heat flux across the end-wall of the duct, but also by the spatial distribution of the heat fluxes.
UR - http://www.scopus.com/inward/record.url?scp=85075444113&partnerID=8YFLogxK
U2 - 10.1115/gt2019-90191
DO - 10.1115/gt2019-90191
M3 - Conference contribution
AN - SCOPUS:85075444113
T3 - Proceedings of the ASME Turbo Expo
BT - Turbomachinery
PB - American Society of Mechanical Engineers(ASME)
T2 - ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition, GT 2019
Y2 - 17 June 2019 through 21 June 2019
ER -