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Transonic Compressor Cascade Flow with Shock Induced Boundary Layer Separation

Fuchs, R. (1991) Transonic Compressor Cascade Flow with Shock Induced Boundary Layer Separation. Euromech 274, Prag, 08.-11.04.91 Videofilm!.

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Item URL in elib:https://elib.dlr.de/37743/
Document Type:Conference or Workshop Item (Speech)
Additional Information: LIDO-Berichtsjahr=1991,
Title:Transonic Compressor Cascade Flow with Shock Induced Boundary Layer Separation
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Fuchs, R.UNSPECIFIEDUNSPECIFIED
Date:1991
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Event Title:Euromech 274, Prag, 08.-11.04.91 Videofilm!
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:other
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:no assignment
DLR - Research theme (Project):UNSPECIFIED
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology
Deposited By: DLR-Beauftragter, elib
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 10:11

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