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Influence of a Downstream Located Obstacle on Transonic Turbine Cascade Flow
Szumowski, A.P. and Amecke, J. and Agocs, J. (1998) Influence of a Downstream Located Obstacle on Transonic Turbine Cascade Flow. International Journal of Turbo and Jet Engines, 15, pp. 27-41.
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Abstract
The effect of a downstream obstacle (rod of 10 mm diameter) on a turbine blade channel flow is investigated experimentally. Variations of the blade life coefficent in function of the rod location are determined. The flow is visualised by means of the schlieren method. Large differences of the channel and corresponding pressure distributions in the trailing part of the blade surface are noted due to the flow-obstacle interaction
| Document Type: | Article | ||||||||
|---|---|---|---|---|---|---|---|---|---|
| Additional Information: | LIDO-Berichtsjahr=1999, | ||||||||
| Title: | Influence of a Downstream Located Obstacle on Transonic Turbine Cascade Flow | ||||||||
| Authors: |
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| Date: | 1998 | ||||||||
| Journal or Publication Title: | International Journal of Turbo and Jet Engines | ||||||||
| Refereed publication: | Yes | ||||||||
| In ISI Web of Science: | Yes | ||||||||
| Volume: | 15 | ||||||||
| Page Range: | pp. 27-41 | ||||||||
| Status: | Published | ||||||||
| Keywords: | Transonic Turbine Cascade, Unsteady Flow, Rotor Stator Interaction | ||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||
| HGF - Program: | Aeronautics | ||||||||
| HGF - Program Themes: | L - no assignement | ||||||||
| DLR - Research area: | Aeronautics | ||||||||
| DLR - Program: | L TT - Triebwerkstechnologien | ||||||||
| DLR - Research theme (Project): | UNSPECIFIED | ||||||||
| Location: | Köln-Porz , Braunschweig , Göttingen | ||||||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > Institut für Strömungsmechanik | ||||||||
| Deposited By: | elib DLR-Beauftragter | ||||||||
| Deposited On: | 16 Sep 2005 | ||||||||
| Last Modified: | 14 Jan 2010 20:25 |
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