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THE EFFECT OF AN ERODED LEADING EDGE ON THE AERODYNAMIC PERFOMANCE 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 PERFOMANCE OF A TRANSONIC FAN BLADE CASCADE. In: ASME Turbo Expo. ASME Turbo Expo, 16.-20. Juni 2014, Düsseldorf, Germany.

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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 PERFOMANCE OF A TRANSONIC FAN BLADE CASCADE
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hergt, Alexanderalexander.hergt (at) dlr.deUNSPECIFIED
Klinner, Joachimjoachim.klinner (at) dlr.deUNSPECIFIED
Steinert, WolfgangDLR-ATUNSPECIFIED
Grund, SebastianDLR-ATUNSPECIFIED
Giebmanns, AngelaDLR-ATUNSPECIFIED
Schnell, RainerAT-FUVUNSPECIFIED
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
Status:Published
Keywords:Eroded leading edge
Event Title:ASME Turbo Expo
Event Location:Düsseldorf, Germany
Event Type:international Conference
Event Dates:16.-20. Juni 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
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Fan and Compressor
Deposited By: Hergt, Dr.-Ing. Alexander Silvio
Deposited On:16 Sep 2014 15:04
Last Modified:09 Feb 2017 19:20

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