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Effects of Reynolds Number and Free-Stream Turbulence on Boundary Layer Transition in a Compressor Cascade - 2000 Heat Transfer Commitee Best Paper

Schreiber, H. A. and Steinert, W. and Küsters, B. (2002) Effects of Reynolds Number and Free-Stream Turbulence on Boundary Layer Transition in a Compressor Cascade - 2000 Heat Transfer Commitee Best Paper. ASME Journal of Turbomachinery, Vol. 124, Janurary 2002, pp. 1-9.

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Item URL in elib:https://elib.dlr.de/1313/
Document Type:Article
Additional Information: LIDO-Berichtsjahr=2005,
Title:Effects of Reynolds Number and Free-Stream Turbulence on Boundary Layer Transition in a Compressor Cascade - 2000 Heat Transfer Commitee Best Paper
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schreiber, H. A.UNSPECIFIEDUNSPECIFIED
Steinert, W.UNSPECIFIEDUNSPECIFIED
Küsters, B.UNSPECIFIEDUNSPECIFIED
Date:2002
Journal or Publication Title:ASME Journal of Turbomachinery
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:Yes
Volume:Vol. 124, Janurary 2002
Page Range:pp. 1-9
Status:Published
Keywords:Boundary layer transition, free-stream turbulence
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: Schreiber, Herr Heinz-Adolf
Deposited On:16 Sep 2005
Last Modified:06 Jan 2010 13:36

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