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Experimental Investigation of Two Exit Guide Vane Cascades Optimized for Operation at Low Reynolds Numbers - ES-OGV-10 and OGV-MOGA-138

Schreiber, H. A. and Steinert, W. (2002) Experimental Investigation of Two Exit Guide Vane Cascades Optimized for Operation at Low Reynolds Numbers - ES-OGV-10 and OGV-MOGA-138. Project Report, DLR-Interner Bericht. DLR IB - 325-03-02, 425 S.

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Document Type:Monograph (Project Report, DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=2005,
Title:Experimental Investigation of Two Exit Guide Vane Cascades Optimized for Operation at Low Reynolds Numbers - ES-OGV-10 and OGV-MOGA-138
Authors:
AuthorsInstitution or Email of Authors
Schreiber, H. A.UNSPECIFIED
Steinert, W.UNSPECIFIED
Date:2002
Number of Pages:425
Status:Published
Keywords:Compressor airfoils, low Reynolds number, cascade tests
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L TT - Triebwerkstechnologien
DLR - Research theme (Project):L - Fan and Compressor Technologies
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology
Deposited By: Herr Heinz-Adolf Schreiber
Deposited On:16 Sep 2005
Last Modified:06 Jan 2010 13:36

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