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Transonic Compressor Rotor Cascade with Boundary-Layer Separation: Experimental and Theoretical Results

Fuchs, R. and Steinert, W. and Starken, H. (1993) Transonic Compressor Rotor Cascade with Boundary-Layer Separation: Experimental and Theoretical Results. The American Society of Mechanical Engineers, NEW York, USA. International Gas Turbine and Aeroengine Congress and Exposition Cincinnaiti,Ohio, May 24-27, 1993, ASME Paper 93-GT-405.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/37877/
Document Type:Conference or Workshop Item (Paper)
Additional Information: institution=ASME, LIDO-Berichtsjahr=1993, pages=9,
Title:Transonic Compressor Rotor Cascade with Boundary-Layer Separation: Experimental and Theoretical Results
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Fuchs, R.UNSPECIFIEDUNSPECIFIED
Steinert, W.UNSPECIFIEDUNSPECIFIED
Starken, H.UNSPECIFIEDUNSPECIFIED
Date:1993
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Publisher:The American Society of Mechanical Engineers, NEW York, USA
Series Name:93-GT-405
Status:Published
Event Title:International Gas Turbine and Aeroengine Congress and Exposition Cincinnaiti,Ohio, May 24-27, 1993, ASME Paper 93-GT-405
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:27 Apr 2009 10:16

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