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Effects of Reynolds Number and free-stream Turbulence on Boundary Layer Transition in a Compressor Cascade

Schreiber, H.-A. and Steinert, W. and Küsters, B. (2000) Effects of Reynolds Number and free-stream Turbulence on Boundary Layer Transition in a Compressor Cascade. International Gas Turbine and Aeroengine Technical Congress, München, Germany, 8.-11. May, 2000.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/1024/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2000,
Title:Effects of Reynolds Number and free-stream Turbulence on Boundary Layer Transition in a Compressor Cascade
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Schreiber, H.-A.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Steinert, W.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Küsters, B.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:2000
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
ASME, UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Series Name:ASME Paper 200-GT-263
Status:Published
Event Title:International Gas Turbine and Aeroengine Technical Congress, München, Germany, 8.-11. May, 2000
Organizer:ASME
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L TT - Triebwerkstechnologien
DLR - Research theme (Project):L - Fan and Compressor Technologies (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology
Deposited By: DLR-Beauftragter, elib
Deposited On:16 Sep 2005
Last Modified:06 Jan 2010 13:10

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