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Compressor Cascade flow with Strong Shock/Wave/Boundary-Layer Interaction

Küsters, B. and Schreiber, H.-A. (1998) Compressor Cascade flow with Strong Shock/Wave/Boundary-Layer Interaction. AIAA Journal, 36 (11), pp. 2072-2078.

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Document Type:Article
Additional Information: LIDO-Berichtsjahr=1999,
Title:Compressor Cascade flow with Strong Shock/Wave/Boundary-Layer Interaction
Authors:
AuthorsInstitution or Email of Authors
Küsters, B.UNSPECIFIED
Schreiber, H.-A.UNSPECIFIED
Date:1998
Journal or Publication Title:AIAA Journal
Refereed publication:Yes
In ISI Web of Science:Yes
Volume:36
Page Range:pp. 2072-2078
Status:Published
Keywords:transsonischer Verdichter, Stoß-Grenzschicht-Interferenz
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:other
HGF - Program Themes:E - no assignement
DLR - Research area:Aeronautics
DLR - Program:E - no assignement
DLR - Research theme (Project):UNSPECIFIED
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 12:59

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