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DETAILED FLOW ANALYSIS OF A COMPRESSOR CASCADE WITH A NON-AXISYMMETRIC ENDWALL CONTOUR

Hergt, Alexander and Klinner, Joachim and Steinert, Wolfgang and Dorfner, Christian and Nicke, Eberhard (2011) DETAILED FLOW ANALYSIS OF A COMPRESSOR CASCADE WITH A NON-AXISYMMETRIC ENDWALL CONTOUR. 9th ETC , 21.-25. March, 2011, Istanbul, Turkey.

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Item URL in elib:https://elib.dlr.de/71629/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:DETAILED FLOW ANALYSIS OF A COMPRESSOR CASCADE WITH A NON-AXISYMMETRIC ENDWALL CONTOUR
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hergt, AlexanderDLRUNSPECIFIED
Klinner, JoachimDLRUNSPECIFIED
Steinert, WolfgangDLRUNSPECIFIED
Dorfner, ChristianEADSUNSPECIFIED
Nicke, EberhardDLRUNSPECIFIED
Date:March 2011
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Non-axisymetric Endwall Contour, Secondary Flow, Compressor Cascade
Event Title:9th ETC
Event Location:Istanbul, Turkey
Event Type:international Conference
Event Dates:21.-25. March, 2011
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Propulsion Systems (old)
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Fan and Compressor Technologies (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Fan and Compressor > Fan and Compressor Technology
Institute of Propulsion Technology > Fan and Compressor
Deposited By: Hergt, Dr.-Ing. Alexander Silvio
Deposited On:17 Nov 2011 08:23
Last Modified:17 Nov 2011 08:23

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