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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.

Full text not available from this repository.

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.

Item URL in elib:https://elib.dlr.de/1290/
Document Type:Article
Additional Information: LIDO-Berichtsjahr=2004,
Title:Experimental Turbine Research at DLR Göttingen
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Kost, F.UNSPECIFIEDUNSPECIFIED
Gieß, P.-A.UNSPECIFIEDUNSPECIFIED
Date:2004
Journal or Publication Title:Journal of the Gas Turbine Society of Japan
Refereed publication:No
Open Access:No
Gold Open Access: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 (old)
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Turbine Technologies (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology
Deposited By: DLR-Beauftragter, elib
Deposited On:16 Sep 2005
Last Modified:06 Jan 2010 13:33

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