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3D Transonic Flow in a Compressor Cascade with Shock-Induced Corner Stall

Weber, A. and Schreiber, H.A. and Fuchs. R., and Steinert, W. (2001) 3D Transonic Flow in a Compressor Cascade with Shock-Induced Corner Stall. In: ASME Turbo Expo 2001, pp. 1-12. ASME Turbo Expo 2001, New Orleans, USA, June 4-7, 2001.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/1107/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2001, monograph_id=2001-GT-345,
Title:3D Transonic Flow in a Compressor Cascade with Shock-Induced Corner Stall
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Weber, A.UNSPECIFIEDUNSPECIFIED
Schreiber, H.A.UNSPECIFIEDUNSPECIFIED
Fuchs. R., UNSPECIFIEDUNSPECIFIED
Steinert, W.UNSPECIFIEDUNSPECIFIED
Date:2001
Journal or Publication Title:ASME Turbo Expo 2001
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1-12
Editors:
EditorsEmail
The American Society of Mechanical Engineers, Atlanta, USA, UNSPECIFIED
Status:Published
Event Title:ASME Turbo Expo 2001, New Orleans, USA, June 4-7, 2001
Organizer:ASME
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:other
HGF - Program Themes:E - no assignment
DLR - Research area:Aeronautics
DLR - Program:E - no assignment
DLR - Research theme (Project):UNSPECIFIED
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology
Deposited By: DLR-Beauftragter, elib
Deposited On:16 Sep 2005
Last Modified:06 Jan 2010 13:18

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