2022
DOI: 10.1016/j.jeurceramsoc.2021.11.044
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Size effect of carbon fiber-reinforced silicon carbide composites (C/C-SiC): Part 2 - tensile testing with alignment device

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Cited by 10 publications
(3 citation statements)
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“…This dichotomy between the promise of 3D printing and its current limitations underscores the critical importance of comprehending the size effect. This becomes especially relevant when considering that numerous materials, ranging from silicon carbide (SiC) ceramics [11] to sea ice [12], composites [13], steel [14], vinyl foam [15], concrete [16], rock [17], lime [18], and an array of polymers [19], exhibit characteristics that are contingent on size. This phenomenon poses a formidable challenge to the scientific community, emphasizing the pressing need for systematic investigations into size effects in additively manufactured polymers.…”
Section: Introductionmentioning
confidence: 99%
“…This dichotomy between the promise of 3D printing and its current limitations underscores the critical importance of comprehending the size effect. This becomes especially relevant when considering that numerous materials, ranging from silicon carbide (SiC) ceramics [11] to sea ice [12], composites [13], steel [14], vinyl foam [15], concrete [16], rock [17], lime [18], and an array of polymers [19], exhibit characteristics that are contingent on size. This phenomenon poses a formidable challenge to the scientific community, emphasizing the pressing need for systematic investigations into size effects in additively manufactured polymers.…”
Section: Introductionmentioning
confidence: 99%
“…1 C f /C, SiC f /C, and C f /SiC have been considered to replace alloys owing to their high melting points (>2700 • C), low density, and high strength. [23][24][25][26][27][28] However, C and SiC tend to oxidize to form CO 2 and SiO 2 , respectively, in environments containing high-temperature air, preventing the direct application of CMCs in aviation and gas turbine engines. To protect CMCs from damage caused by hightemperature air or steam, environmental barrier coatings (EBCs) have been proposed, which delay their oxidization and thus lower the probability of their failure.…”
Section: Introductionmentioning
confidence: 99%
“…Currently, the working temperature is limited to approximately 1150°C for Ni‐based alloys, in which TBCs with a thickness of approximately 300–500 μm can provide a temperature gradient of 50–150°C under the effects of cooling air 1,16,17,19–22 . Ceramic matrix composites (CMCs), such as SiC f /SiC (where the subscript f represents fibers), C f /C, SiC f /C, and C f /SiC have been considered to replace alloys owing to their high melting points (>2700°C), low density, and high strength 23–28 . However, C and SiC tend to oxidize to form CO 2 and SiO 2 , respectively, in environments containing high‐temperature air, preventing the direct application of CMCs in aviation and gas turbine engines.…”
Section: Introductionmentioning
confidence: 99%