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Investigation of flow phenomena and heat transfer performance of a ribbed two-pass cooling channel with turbine typical cross sections

Schubert, S. and Neumann, S.O. and Jarius, M. and Elfert, M. and Weigand, B. (2003) Investigation of flow phenomena and heat transfer performance of a ribbed two-pass cooling channel with turbine typical cross sections. In: Proceedings. 16th Intern.Symp. on Air Breathing Engines,Aug.31-Sept.5,2003,Cleveland,Ohio,USA.

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Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2004,
Title:Investigation of flow phenomena and heat transfer performance of a ribbed two-pass cooling channel with turbine typical cross sections
Authors:
AuthorsInstitution or Email of Authors
Schubert, S.UNSPECIFIED
Neumann, S.O.UNSPECIFIED
Jarius, M.UNSPECIFIED
Elfert, M.UNSPECIFIED
Weigand, B.UNSPECIFIED
Date:2003
Journal or Publication Title:Proceedings
Status:Published
Event Title:16th Intern.Symp. on Air Breathing Engines,Aug.31-Sept.5,2003,Cleveland,Ohio,USA
Organizer:ISABE
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 - Virtual Engine and Validation Methods
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology
Deposited By: Herr Richard Schodl
Deposited On:16 Sep 2005
Last Modified:06 Jan 2010 13:33

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