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Design, Manufacture and Instrumentation of Cascade and Cooling Blades at DLR (European Research Project AITEB-2)

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.

Full text not available from this repository.

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/
Document Type:Monograph (DLR-Interner Bericht)
Title:Design, Manufacture and Instrumentation of Cascade and Cooling Blades at DLR (European Research Project AITEB-2)
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Rehder, Hans-JürgenUNSPECIFIEDUNSPECIFIED
Date:December 2006
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science: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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