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A Proposed Explanation of the Butterfly-Shaped Delamination Cracks Obtained by Means of Rockwell Indentation on TBC Systems with Anisotropic Substrate

Mircea, I. (2004) A Proposed Explanation of the Butterfly-Shaped Delamination Cracks Obtained by Means of Rockwell Indentation on TBC Systems with Anisotropic Substrate. SICMAC Meeting, DLR Köln, 12.03.2004.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/17663/
Document Type:Conference or Workshop Item (Speech)
Additional Information: LIDO-Berichtsjahr=2004,
Title:A Proposed Explanation of the Butterfly-Shaped Delamination Cracks Obtained by Means of Rockwell Indentation on TBC Systems with Anisotropic Substrate
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Mircea, I.UNSPECIFIEDUNSPECIFIED
Date:2004
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Event Title:SICMAC Meeting, DLR Köln, 12.03.2004
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):UNSPECIFIED
Location: Köln-Porz
Institutes and Institutions:Institute of Materials Research
Deposited By: DLR-Beauftragter, elib
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 18:06

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