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Close to reality testing of gas turbine blade materials – the thermal gradient mechanical fatigue test

Bartsch, Marion (2006) Close to reality testing of gas turbine blade materials – the thermal gradient mechanical fatigue test. Seminar for graduate and undergraduate students, 2006-05-10, Newark, DE, USA.

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Item URL in elib:https://elib.dlr.de/45999/
Document Type:Conference or Workshop Item (Speech)
Title:Close to reality testing of gas turbine blade materials – the thermal gradient mechanical fatigue test
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Bartsch, MarionUNSPECIFIEDUNSPECIFIED
Date:10 May 2006
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:advanced testing, thermal mechanical fatigue, damage mechanisms
Event Title:Seminar for graduate and undergraduate students
Event Location:Newark, DE, USA
Event Type:Other
Event Dates:2006-05-10
Organizer:Department of Mechanical Engineering, University of Delaware
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Propulsion Systems (old)
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Virtual Engine and Validation Methods (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Materials Research
Deposited By: Bartsch, Dr.-Ing. Marion
Deposited On:06 Dec 2006
Last Modified:27 Apr 2009 13:18

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