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Advanced High-Turning Compressor Airfoils for Low Reynolds Number Condition - Part II: Experimental and Numerical Analysis

Schreiber, H. A. and Steinert, W. and Sonoda, T. and Arima, T. (2004) Advanced High-Turning Compressor Airfoils for Low Reynolds Number Condition - Part II: Experimental and Numerical Analysis. ASME Journal of Turbomachinery, Vol. 126, October 2004, pp. 482-492.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/1309/
Document Type:Article
Additional Information: LIDO-Berichtsjahr=2005,
Title:Advanced High-Turning Compressor Airfoils for Low Reynolds Number Condition - Part II: Experimental and Numerical Analysis
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schreiber, H. A.UNSPECIFIEDUNSPECIFIED
Steinert, W.UNSPECIFIEDUNSPECIFIED
Sonoda, T.UNSPECIFIEDUNSPECIFIED
Arima, T.UNSPECIFIEDUNSPECIFIED
Date:2004
Journal or Publication Title:ASME Journal of Turbomachinery
Refereed publication:Yes
Open Access:Yes
Gold Open Access:Yes
In SCOPUS:No
In ISI Web of Science:Yes
Volume:Vol. 126, October 2004
Page Range:pp. 482-492
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:12 Mar 2010 13:48

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