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Experimental Turbine Research at DLR Göttingen

Kost, F. and Gieß, P.-A. (2004) Experimental Turbine Research at DLR Göttingen. Journal of the Gas Turbine Society of Japan, Vol. 32 (No. 6), pp. 47-56.

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Abstract

At DLR Goettingen (Germany) two windtunnels especially adapted to turbine research in the transonic flow regime are available. These are the “Windtunnel for Straight Cascades” and the “Windtunnel for Rotating Cascades”. The Straight Cascade windtunnel is of blow-down type, operating in the Mach number range of 0.2 to 1.6. The Rotating Cascade Tunnel is a facility with closed flow path enabling the independent variation of Mach and Reynolds number. In the Rotating Cascade Tunnel the investigated objects range from isolated vanes to 1½ stages. In the following the features of the windtunnels will be described and some experimental results shown.

Document Type:Article
Additional Information: LIDO-Berichtsjahr=2004,
Title:Experimental Turbine Research at DLR Göttingen
Authors:
AuthorsInstitution or Email of Authors
Kost, F.UNSPECIFIED
Gieß, P.-A.UNSPECIFIED
Date:2004
Journal or Publication Title:Journal of the Gas Turbine Society of Japan
Refereed publication:No
In SCOPUS:No
In ISI Web of Science:No
Volume:Vol. 32
Page Range:pp. 47-56
Status:Published
Keywords:Turbomachinery, Turbine, Aerodynamics, Transonic Flow, Heat Transfer, Windtunnel, Cascade, Measurement Techniques
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 13:33

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