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Rehder, Hans-Jürgen (2006) Design, Manufacture and Instrumentation of Cascade and Cooling Blades at DLR (European Research Project AITEB-2). DLR-Interner Bericht. IB 225-2006 A 07.
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Abstract
This report describes design, manufacturing and instrumentation of a linear cascade consisting of high pressure turbine blades with three different trailing edge cooling configurations, which were built up for aerodynamic erformance experiments in the transonic cascade wind tunnel at DLR. The investigations are performed within Work Package 2 of the 6th Framework Project AITEB-2
| Item URL in elib: | https://elib.dlr.de/46151/ | ||||||||
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| Document Type: | Monograph (DLR-Interner Bericht) | ||||||||
| Title: | Design, Manufacture and Instrumentation of Cascade and Cooling Blades at DLR (European Research Project AITEB-2) | ||||||||
| Authors: |
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| Date: | December 2006 | ||||||||
| Open Access: | No | ||||||||
| Status: | Published | ||||||||
| Keywords: | linear cascade wind tunnel, high pressure turbine cascade, coolant ejection, trailing edge geometry, coolant blade design | ||||||||
| HGF - Research field: | Aeronautics, Space and Transport (old) | ||||||||
| HGF - Program: | Aeronautics | ||||||||
| HGF - Program Themes: | Propulsion Systems (old) | ||||||||
| DLR - Research area: | Aeronautics | ||||||||
| DLR - Program: | L ER - Engine Research | ||||||||
| DLR - Research theme (Project): | L - Turbine Technologies (old) | ||||||||
| Location: | Göttingen | ||||||||
| Institutes and Institutions: | Institute of Propulsion Technology > Turbine | ||||||||
| Deposited By: | Klein, Stephanie | ||||||||
| Deposited On: | 11 Dec 2006 | ||||||||
| Last Modified: | 27 Apr 2009 13:19 |
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