2017
DOI: 10.1016/j.jeurceramsoc.2016.09.030
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Strain field evolution of 2D needled C/SiC composites under tension

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Cited by 20 publications
(2 citation statements)
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“…Silicon–carbon–fiber‐reinforced silicon carbide matrix composites (SiC f /SiC) are regarded as one of the most promising materials for aircraft hot section components due to their excellent mechanical properties in high‐temperature environments 1–9 . When assembling complex high‐temperature section components, ceramic–matrix composites (CMCs) joints with high mechanical properties are used to ensure the structural strength of the joint 10,11 .…”
Section: Introductionmentioning
confidence: 99%
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“…Silicon–carbon–fiber‐reinforced silicon carbide matrix composites (SiC f /SiC) are regarded as one of the most promising materials for aircraft hot section components due to their excellent mechanical properties in high‐temperature environments 1–9 . When assembling complex high‐temperature section components, ceramic–matrix composites (CMCs) joints with high mechanical properties are used to ensure the structural strength of the joint 10,11 .…”
Section: Introductionmentioning
confidence: 99%
“…Silicon-carbon-fiber-reinforced silicon carbide matrix composites (SiC f /SiC) are regarded as one of the most promising materials for aircraft hot section components due to their excellent mechanical properties in hightemperature environments. [1][2][3][4][5][6][7][8][9] When assembling complex high-temperature section components, ceramic-matrix composites (CMCs) joints with high mechanical properties are used to ensure the structural strength of the joint. 10,11 The 2D CMCs z-pinned joint is a mechanical joint with excellent performance, which could be widely used in the connection of complex aircraft thermal sections in the future.…”
Section: Introductionmentioning
confidence: 99%