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Experimental investigation of four compressor blade sections in the Transonik Cascade Facility (TGK) of DLR Cologne, Final Report

Schreiber, H.A. and Steiner, W. (2006) Experimental investigation of four compressor blade sections in the Transonik Cascade Facility (TGK) of DLR Cologne, Final Report. Other. DLR-Interner Bericht. DLR IB-325-06-06. (Unpublished)

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Document Type:Monograph (DLR-Interner Bericht, Other)
Title:Experimental investigation of four compressor blade sections in the Transonik Cascade Facility (TGK) of DLR Cologne, Final Report
Authors:
AuthorsInstitution or Email of Authors
Schreiber, H.A.UNSPECIFIED
Steiner, W.UNSPECIFIED
Date:June 2006
Status:Unpublished
Keywords:Stationäre Gasturbine, Verdichtergitter, Transonischer Verdichter
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 > Fan and Compressor
Deposited By: Rosemarie Fox
Deposited On:18 Aug 2006
Last Modified:27 Apr 2009 13:01

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