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Advanced Nonaxisymmetric Endwall Contouring for Axial Compressors by Generating an Aerodynamic Separator—Part II: Experimental and Numerical Cascade Investigation

Hergt, Alexander and Dorfner, Christian and Steinert, Wolfgang and Nicke, Eberhard and Schreiber, Heinz-Adolf (2011) Advanced Nonaxisymmetric Endwall Contouring for Axial Compressors by Generating an Aerodynamic Separator—Part II: Experimental and Numerical Cascade Investigation. Journal of Turbomachinery, Vol. 133 (021027), pp. 1-8. American Society of Mechanical Engineers (ASME). DOI: DOI: 10.1115/1.4001224

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Item URL in elib:https://elib.dlr.de/71633/
Document Type:Article
Title:Advanced Nonaxisymmetric Endwall Contouring for Axial Compressors by Generating an Aerodynamic Separator—Part II: Experimental and Numerical Cascade Investigation
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hergt, AlexanderDLRUNSPECIFIED
Dorfner, ChristianEADSUNSPECIFIED
Steinert, WolfgangDLRUNSPECIFIED
Nicke, EberhardDLRUNSPECIFIED
Schreiber, Heinz-AdolfDLRUNSPECIFIED
Date:2011
Journal or Publication Title:Journal of Turbomachinery
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:Vol. 133
DOI :DOI: 10.1115/1.4001224
Page Range:pp. 1-8
Publisher:American Society of Mechanical Engineers (ASME)
Status:Published
Keywords:Non-Axisymetric Endwall Contour, Secondary Flow, Compressor Cascade
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 08:22
Last Modified:08 Mar 2018 18:46

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