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DLR Rig Instrumentation -European Research Project AITEB-

Rehder, H.-J. and Dannhauer, A. (2004) DLR Rig Instrumentation -European Research Project AITEB-. DLR-Interner Bericht, Project Report. 225-2004 A 08.

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Abstract

This report gives an overview of the new DLR cascade test rig and its instrumentation, which was designed and built up for experimental investigations within work package 3 of the framework V project AITEB. The wind tunnel equipment for flow field and heat transfer measurements is described in detail. Measurement locations in the test section, overall boundary conditions and experimental parameters / geometries to be studied are also presented.

Document Type:Monograph (DLR-Interner Bericht, Project Report)
Additional Information: LIDO-Berichtsjahr=2004,
Title:DLR Rig Instrumentation -European Research Project AITEB-
Authors:
AuthorsInstitution or Email of Authors
Rehder, H.-J.UNSPECIFIED
Dannhauer, A.UNSPECIFIED
Date:2004
Status:Published
Keywords:nozzle guide vanes, shrouded vanes, linear cascade, tip platform,
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Propulsion Systems
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Turbine Technologies
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology
Deposited By: elib DLR-Beauftragter
Deposited On:16 Sep 2005
Last Modified:06 Jan 2010 13:31

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