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The Effect of an Eroded Leading Edge on the Aerodynamic Performance of a Transonic Fan Blade Cascade

Hergt, Alexander and Klinner, Joachim and Steinert, Wolfgang and Grund, Sebastian and Giebmanns, Angela and Schnell, Rainer (2014) The Effect of an Eroded Leading Edge on the Aerodynamic Performance of a Transonic Fan Blade Cascade. In: ASME Turbo Expo. ASME Turbo Expo, 2014-06-16 - 2014-06-20, Düsseldorf, Germany. doi: 10.1115/GT2014-25023.

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Item URL in elib:https://elib.dlr.de/90604/
Document Type:Conference or Workshop Item (Speech)
Additional Information:GT2014-25023
Title:The Effect of an Eroded Leading Edge on the Aerodynamic Performance of a Transonic Fan Blade Cascade
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Hergt, AlexanderUNSPECIFIEDhttps://orcid.org/0009-0008-1643-7326UNSPECIFIED
Klinner, JoachimUNSPECIFIEDhttps://orcid.org/0000-0003-2709-9664UNSPECIFIED
Steinert, WolfgangDLR-ATUNSPECIFIEDUNSPECIFIED
Grund, SebastianDLR-ATUNSPECIFIEDUNSPECIFIED
Giebmanns, AngelaDLR-ATUNSPECIFIEDUNSPECIFIED
Schnell, RainerAT-FUVUNSPECIFIEDUNSPECIFIED
Date:June 2014
Journal or Publication Title:ASME Turbo Expo
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:Yes
DOI:10.1115/GT2014-25023
Status:Published
Keywords:Eroded leading edge
Event Title:ASME Turbo Expo
Event Location:Düsseldorf, Germany
Event Type:international Conference
Event Start Date:16 June 2014
Event End Date:20 June 2014
Organizer:ASME
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:propulsion systems
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
Deposited By: Hergt, Dr.-Ing. Alexander
Deposited On:16 Sep 2014 15:04
Last Modified:24 Apr 2024 19:56

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