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Inlet flow angle determination of transonic compressor cascade

Steinert, W. and Fuchs, R. and Starken, H. (1991) Inlet flow angle determination of transonic compressor cascade. 36th ASME International Gas Turbine and Aeroengine Congress and Exposition, Orlando (USA), 03.-06.06.91.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/37748/
Document Type:Conference or Workshop Item (Speech)
Additional Information: LIDO-Berichtsjahr=1991,
Title:Inlet flow angle determination of transonic compressor cascade
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Steinert, W.UNSPECIFIEDUNSPECIFIED
Fuchs, R.UNSPECIFIEDUNSPECIFIED
Starken, H.UNSPECIFIEDUNSPECIFIED
Date:1991
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Event Title:36th ASME International Gas Turbine and Aeroengine Congress and Exposition, Orlando (USA), 03.-06.06.91
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L SI - Versuchs- und Simulationstechniken
DLR - Research theme (Project):UNSPECIFIED
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology
Deposited By: DLR-Beauftragter, elib
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 10:12

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