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An Investigation of a Strong Shock-Wave Turbulent Boundary Layer Interaction in a Supersonic Compressor Cascade

Schreiber, H.A. and Starken, H. (1992) An Investigation of a Strong Shock-Wave Turbulent Boundary Layer Interaction in a Supersonic Compressor Cascade. Transaction of the ASME, Journal of Turbomachinery July 1992, Vol.14, pp.494-503, pp. 949-503.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/37793/
Document Type:Article
Additional Information: institution=SM-AT/ASME, LIDO-Berichtsjahr=1992, pages=10,
Title:An Investigation of a Strong Shock-Wave Turbulent Boundary Layer Interaction in a Supersonic Compressor Cascade
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schreiber, H.A. UNSPECIFIEDUNSPECIFIED
Starken, H. UNSPECIFIEDUNSPECIFIED
Date:1992
Journal or Publication Title:Transaction of the ASME, Journal of Turbomachinery July 1992, Vol.14, pp.494-503
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:Yes
Page Range:pp. 949-503
Status:Published
HGF - Research field:UNSPECIFIED
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:L TT - Triebwerkstechnologien
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:26 Feb 2010 14:50

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