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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.

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Abstract

Compressor Airfoils, low Reynolds number

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 Authors
Sonoda, T.UNSPECIFIED
Yamaguchi, Y.UNSPECIFIED
Arima,, UNSPECIFIED
Olhofer, M.UNSPECIFIED
Sendhoff, B.UNSPECIFIED
Schreiber, H. A.UNSPECIFIED
Date:2003
Journal or Publication Title:ASME Turbo Expo 2003
Editors:
EditorsEmail
The American Society of Mechanical Engineers, UNSPECIFIED
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: Herr Heinz-Adolf Schreiber
Deposited On:16 Sep 2005
Last Modified:06 Jan 2010 13:36

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