Hofmann, Severin und Koch, Dietmar und Voggenreiter, Heinz (2012) Modelling the Bending Test Behaviour of Carbon Fibre Reinforced SiC by Finite Element Method. In: Proceedings of the 12th European Conference on Spacecraft Structrues, Materials and Environmental Testing on DVD. 12th European Conference on Spacecraft Structures, Materials & Environmental Testing, 2012-03-20 - 2012-03-23, Noordwijk, Niederlande.
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Kurzfassung
Liquid silicon infiltrated carbon fibre reinforced SiC, has shown to be a high-potential material for thermal protection systems. The tensile and bending behaviour of the ceramic-matrix composite, C/C-SiC, were investigated in varying orientations relative to the 0/90° woven carbon fibres. The ratio of bending to tensile strength was about 1.7 to 2 depending on the loading direction. With the goal to understand this large difference finite element analyses (FEA) of the bending tests were performed. The different stress-strain behaviour of C/C-SiC under tensile and compression load were included in the FEA. Additionally the bending failure of the CMC-material was modelled by Cohesive Zone Elements (CZE) accounting for the directional tensile strength and Work of Fracture (WOF). The WOF was determined by Single Edge Notched Bending (SENB) tests. Comparable results from FEA and bending test were achieved. The presented approach could also be adapted for the design of C/C-SiC-components and structures.
elib-URL des Eintrags: | https://elib.dlr.de/79422/ | ||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag, Paper) | ||||||||||||||||
Titel: | Modelling the Bending Test Behaviour of Carbon Fibre Reinforced SiC by Finite Element Method | ||||||||||||||||
Autoren: |
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Datum: | 20 März 2012 | ||||||||||||||||
Erschienen in: | Proceedings of the 12th European Conference on Spacecraft Structrues, Materials and Environmental Testing on DVD | ||||||||||||||||
Open Access: | Nein | ||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||
Stichwörter: | CMC, Work of Fracture, Cohesive Zone, FEA, Bending, Tensile, C/C-SiC | ||||||||||||||||
Veranstaltungstitel: | 12th European Conference on Spacecraft Structures, Materials & Environmental Testing | ||||||||||||||||
Veranstaltungsort: | Noordwijk, Niederlande | ||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||
Veranstaltungsbeginn: | 20 März 2012 | ||||||||||||||||
Veranstaltungsende: | 23 März 2012 | ||||||||||||||||
Veranstalter : | ESA | ||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||
HGF - Programm: | Raumfahrt | ||||||||||||||||
HGF - Programmthema: | Raumtransport | ||||||||||||||||
DLR - Schwerpunkt: | Raumfahrt | ||||||||||||||||
DLR - Forschungsgebiet: | R RP - Raumtransport | ||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | R - Propulsion 2020 / CFD und Simulation (alt) | ||||||||||||||||
Standort: | Stuttgart | ||||||||||||||||
Institute & Einrichtungen: | Institut für Bauweisen- und Konstruktionsforschung > Keramische Verbundstrukturen | ||||||||||||||||
Hinterlegt von: | Hofmann, Severin | ||||||||||||||||
Hinterlegt am: | 17 Dez 2012 15:06 | ||||||||||||||||
Letzte Änderung: | 24 Apr 2024 19:45 |
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