1998
DOI: 10.1111/j.1151-2916.1998.tb02550.x
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Mechanical Behavior and High‐Temperature Performance of a Woven Nicalon™/Si‐N‐C Ceramic‐Matrix Composite

Abstract: A modern ceramic-matrix composite (CMC) has been extensively characterized for a high-temperature aerospace turbine-engine application. The CMC system has a siliconnitrogen-carbon (Si-N-C) matrix reinforced with Nicalon fibers woven in a balanced eight-harness satin weave fabric. Tensile tests have demonstrated that this CMC exhibits excellent strength retention up to 1100°C. The roomtemperature fatigue limit was 160 MPa, ∼80% of the roomtemperature tensile strength. The composite reached runout conditions und… Show more

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Cited by 52 publications
(21 citation statements)
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“…Most SiCfiber-containing CMCs exhibit longer life under static loading and shorter life under cyclic loading [27]. For these materials, fatigue is significantly more damaging than creep.…”
Section: Introductionmentioning
confidence: 99%
“…Most SiCfiber-containing CMCs exhibit longer life under static loading and shorter life under cyclic loading [27]. For these materials, fatigue is significantly more damaging than creep.…”
Section: Introductionmentioning
confidence: 99%
“…Oxide‐oxide composites with porous matrix display behavior tendencies that are markedly different from those reported for the composites with dense SiC‐based matrices and an interface between fibers and matrix. Most SiC/SiC CMCs display longer lifetimes under sustained loads and shorter lifetimes when subjected to cyclic fatigue . For these composites, cyclic loading is substantially more detrimental than sustained loading.…”
Section: Introductionmentioning
confidence: 99%
“…This behavior is very similar to that observed by other authors and supports the suggestion that the initial creep occurs because of load-sharing effects, after which only marginal creep strain occurs. [24][25][26][27] It also implies that a damage mechanism controls the creep of C/C composites. After the saturation of matrixcracking in the first stage of creep, the creep of composite is controlled by a combination of the energy dissipative mechanisms like fiber debonding, fracture and pull-out of the fibers, matrix microcracking, etc.…”
Section: Resultsmentioning
confidence: 99%