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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. (2003) Advanced High-Turning Compressor Airfoils for Low Reynolds Number Condition - Part II: Experimental and Numerical Analysis. In: ASME Turbo Expo 2003, Atlanta, June 16-19. International Gasd Turbine and Aero Engine Congress, Atlanta, June 16-19, 2003.

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Official URL: Compressor Airfoils, low Reynolds number


Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2005, monograph_id=Paper No. 2003-GT-38477,
Title:Advanced High-Turning Compressor Airfoils for Low Reynolds Number Condition - Part II: Experimental and Numerical Analysis
Authors:
AuthorsInstitution or Email of Authors
Schreiber, H. A.UNSPECIFIED
Steinert, W.UNSPECIFIED
Sonoda, T.UNSPECIFIED
Arima, T.UNSPECIFIED
Date:2003
Journal or Publication Title:ASME Turbo Expo 2003, Atlanta, June 16-19
Editors:
EditorsEmail
ASME, The American Society of Mechanical EngineersUNSPECIFIED
Status:Published
Event Title:International Gasd Turbine and Aero Engine Congress, Atlanta, 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):L - Fan and Compressor Technologies
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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