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Experimental Investigations of the Flow Field within a Gas Turbine Rotor Cascade without Coolant Ejektion Designed by RRD. Appendix B.

Ochrymiuk, T. and Gieß, P.-A. and Kost, F. (2004) Experimental Investigations of the Flow Field within a Gas Turbine Rotor Cascade without Coolant Ejektion Designed by RRD. Appendix B. DLR-Interner Bericht. 225 - 2003 C 07 B, 56 S.

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Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=2004,
Title:Experimental Investigations of the Flow Field within a Gas Turbine Rotor Cascade without Coolant Ejektion Designed by RRD. Appendix B.
Authors:
AuthorsInstitution or Email of Authors
Ochrymiuk, T.UNSPECIFIED
Gieß, P.-A.UNSPECIFIED
Kost, F.UNSPECIFIED
Date:2004
Number of Pages:56
Status:Published
Keywords:Gas Turbine
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 13:25

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