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

Sonoda, T. and Yamaguchi, Y. and Arima,, and Olhofer, M. and Sendhoff, B. and Schreiber, H. A. (2003) Advanced High Turning Compressor Airfoils for Low Reynolds Number Conditrion - Part I: Design and Optimization. In: ASME Turbo Expo 2003. International Gas Turbine and Aero Engine Congress, Atlanta, GA, June 16-19, 2003.

Full text not available from this repository.

Abstract

Compressor Airfoils, low Reynolds number

Item URL in elib:https://elib.dlr.de/1316/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2005, monograph_id=Paper No. ASME-GT-38458,
Title:Advanced High Turning Compressor Airfoils for Low Reynolds Number Conditrion - Part I: Design and Optimization
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Sonoda, T.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Yamaguchi, Y.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Arima,, UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Olhofer, M.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Sendhoff, B.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Schreiber, H. A.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:2003
Journal or Publication Title:ASME Turbo Expo 2003
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
The American Society of Mechanical Engineers, UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Status:Published
Event Title:International Gas Turbine and Aero Engine Congress, Atlanta, GA, June 16-19, 2003
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):UNSPECIFIED
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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