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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. (1991) An investigation of a strong shock-wave turbulent boundary layer interaction in a supersonic compressor cascade. presented at the International Gas Turbine and Aeroengine Congress, Orlande (USA), 03.-06.06.91.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/37740/
Document Type:Conference or Workshop Item (Speech)
Additional Information: LIDO-Berichtsjahr=1991,
Title:An investigation of a strong shock-wave turbulent boundary layer interaction in a supersonic compressor cascade
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Schreiber, H.-A.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Starken, H.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:1991
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Event Title:presented at the International Gas Turbine and Aeroengine Congress, Orlande (USA), 03.-06.06.91
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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