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Advanced High Turning Compressor Airfoils for Low Reynolds Number Condition - Part I: Design and Optimization

Sonoda, T. and Yamaguchi, Y. and Arima, T. and Olhofer, M. and Sendhoff, B. and Schreiber, H. A. (2004) Advanced High Turning Compressor Airfoils for Low Reynolds Number Condition - Part I: Design and Optimization. ASME Journal of Turbomachinery, Vol. 126, July 2004, pp. 350-359.

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Item URL in elib:https://elib.dlr.de/1308/
Document Type:Article
Additional Information: LIDO-Berichtsjahr=2005,
Title:Advanced High Turning Compressor Airfoils for Low Reynolds Number Condition - Part I: Design and Optimization
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Sonoda, T.UNSPECIFIEDUNSPECIFIED
Yamaguchi, Y.UNSPECIFIEDUNSPECIFIED
Arima, T.UNSPECIFIEDUNSPECIFIED
Olhofer, M.UNSPECIFIEDUNSPECIFIED
Sendhoff, B.UNSPECIFIEDUNSPECIFIED
Schreiber, H. A.UNSPECIFIEDUNSPECIFIED
Date:2004
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. 126, July 2004
Page Range:pp. 350-359
Status:Published
Keywords:Compressor airfoils, Low Reynolds number
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 13:35

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