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ADVANCED NON-AXISYMMETRIC 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 (2009) ADVANCED NON-AXISYMMETRIC ENDWALL CONTOURING FOR AXIAL COMPRESSORS BY GENERATING AN AERODYNAMIC SEPARATOR - PART II: EXPERIMENTAL AND NUMERICAL CASCADE INVESTIGATION. ASME Turbo Expo 2009, 8.-12. Juni, Orlando.

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Document Type:Conference or Workshop Item (Speech, Paper)
Title:ADVANCED NON-AXISYMMETRIC ENDWALL CONTOURING FOR AXIAL COMPRESSORS BY GENERATING AN AERODYNAMIC SEPARATOR - PART II: EXPERIMENTAL AND NUMERICAL CASCADE INVESTIGATION
Authors:
AuthorsInstitution or Email of Authors
Hergt, Alexanderalexander.hergt@dlr.de
Dorfner, ChristianUNSPECIFIED
Steinert, WolfgangUNSPECIFIED
Nicke, EberhardUNSPECIFIED
Schreiber, Heinz-AdolfUNSPECIFIED
Date:2009
Refereed publication:Yes
In ISI Web of Science:No
Series Name:Proceedings of ASME Turbo Expo 2009 (GT2009-59384)
Status:Published
Keywords:Endwandkontur, Verdichter, Sekundärströmung
Event Title:ASME Turbo Expo 2009
Event Location:Orlando
Event Type:international Conference
Event Dates:8.-12. Juni
Organizer:ASME
HGF - Research field:Energy
HGF - Program:Aeronautics, Efficient Energy Conversion (old)
HGF - Program Themes:Propulsion Systems, Aircraft Research, E VG - Combustion and Gas Turbine Technologies (old)
DLR - Research area:Energy, Aeronautics
DLR - Program:L ER - Engine Research, L TT - Triebwerkstechnologien, L AR - Aircraft Research, E VG - Combustion and Gas Turbine Technologies
DLR - Research theme (Project):L - Flight Physics, E - Gasturbine (old), L - Fan and Compressor Technologies
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Fan and Compressor > Fan and Compressor Technology
Deposited By: Alexander Silvio Hergt
Deposited On:15 Mar 2010 15:37
Last Modified:15 Mar 2010 15:37

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