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

Schreiber, H.A. and Weber, A. and Fuchs, R. and Steinert, W. (2001) 3D Transonic Flow in a Compressor Cascade with Shock-Induced Corner Stall. The 46th ASME International Gas Turbine & Aeroengine Technical Congress, New Orleans, USA, June 4-7, 2001.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/1109/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2001,
Title:3D Transonic Flow in a Compressor Cascade with Shock-Induced Corner Stall
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schreiber, H.A.UNSPECIFIEDUNSPECIFIED
Weber, A.UNSPECIFIEDUNSPECIFIED
Fuchs, R.UNSPECIFIEDUNSPECIFIED
Steinert, W.UNSPECIFIEDUNSPECIFIED
Date:2001
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Event Title:The 46th ASME International Gas Turbine & Aeroengine Technical Congress, New Orleans, USA, June 4-7, 2001
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 (old)
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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