Aoki, R. and Eberle, K. (2000) Damage development in pin loaded C/C-SiC specimens. ICCE-7, Denver, Colorado, 2-8. Juli 2000.
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Continuous fibre reinforced ceramic matrix composites (CMC) are under development for use in advanced structural aerospace and terrestrial applications that require high temperature materials with low density and non-catastrophic failure modes. The C/C-SiC material was manufactured at the DLR after the in-house developed process based on the pyrolysis of high carbonaceous precursors and the liquid silicon infiltration (LSI process). Some results of an ongoing research programme on pin loaded CMC specimens are presented.
|Document Type:||Conference or Workshop Item (Paper)|
|Title:||Damage development in pin loaded C/C-SiC specimens|
|Keywords:||CMC, ceramic, fibre reinforced ceramic, pin loading, NDI, non-destructive testing, mechanical vibration, ultrasonic,|
|Event Title:||ICCE-7, Denver, Colorado, 2-8. Juli 2000|
|Organizer:||International Community for Composites Engineering (ICCE); College of Engineering, University of New Orleans|
|HGF - Research field:||Aeronautics, Space and Transport (old)|
|HGF - Program:||Space (old)|
|HGF - Program Themes:||W RP - Raumtransport|
|DLR - Research area:||Space|
|DLR - Program:||W RP - Raumtransport|
|DLR - Research theme (Project):||UNSPECIFIED|
|Institutes and Institutions:||Institute of Structures and Design|
|Deposited By:||elib DLR-Beauftragter|
|Deposited On:||16 Sep 2005|
|Last Modified:||14 Jan 2010 22:16|
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