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ADVANCED NON-AXISYMMETRIC ENDWALL CONTOURING FOR AXIAL COMPRESSORS BY GENERATING AN AERODYNAMIC SEPARATOR - PART I: PRINCIPAL CASCADE DESIGN AND COMPRESSOR APPLICATION

Dorfner, Christian and Hergt, Alexander and Nicke, Eberhard and Mönig, Reinhard (2009) ADVANCED NON-AXISYMMETRIC ENDWALL CONTOURING FOR AXIAL COMPRESSORS BY GENERATING AN AERODYNAMIC SEPARATOR - PART I: PRINCIPAL CASCADE DESIGN AND COMPRESSOR APPLICATION. ASME Turbo Expo 2009, 2009-06-08 - 2009-06-12, Orlando.

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Item URL in elib:https://elib.dlr.de/63599/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:ADVANCED NON-AXISYMMETRIC ENDWALL CONTOURING FOR AXIAL COMPRESSORS BY GENERATING AN AERODYNAMIC SEPARATOR - PART I: PRINCIPAL CASCADE DESIGN AND COMPRESSOR APPLICATION
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Dorfner, ChristianUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Hergt, AlexanderUNSPECIFIEDhttps://orcid.org/0009-0008-1643-7326UNSPECIFIED
Nicke, EberhardUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Mönig, ReinhardUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:2009
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Series Name:Proceedings of ASME Turbo Expo 2009 (GT2009-59383)
Status:Published
Keywords:Endwandkonturierung, Verdichter, Sekundärströmung
Event Title:ASME Turbo Expo 2009
Event Location:Orlando
Event Type:international Conference
Event Start Date:8 June 2009
Event End Date:12 June 2009
Organizer:ASME
HGF - Research field:Aeronautics, Space and Transport, Energy
HGF - Program:Aeronautics, Efficient Energy Conversion (old)
HGF - Program Themes:Aircraft Research (old), E VG - Combustion and Gas Turbine Technologies (old), Propulsion Systems (old)
DLR - Research area:Aeronautics, Energy
DLR - Program:L AR - Aircraft Research, E VG - Combustion and Gas Turbine Technologies, L ER - Engine Research
DLR - Research theme (Project):L - Flight Physics (old), E - Gasturbine (old), L - Fan and Compressor Technologies (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Fan and Compressor
Deposited By: Hergt, Dr.-Ing. Alexander
Deposited On:15 Mar 2010 15:38
Last Modified:24 Apr 2024 19:28

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