2018
DOI: 10.1016/j.ijfatigue.2018.07.001
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Study of random fatigue behavior of C/SiC composite thin-wall plates

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Cited by 18 publications
(5 citation statements)
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“…However, stochastic load may occur during cyclic-fatigue loading, and cause extra damage in the composite, which affects the values of FLS. 27,28 Wu et al 29 performed experimental investigation on the vibration fatigue behavior of C/SiC composites under random loading. The stochastic vibration overloading degraded the fatigue life and FLS of the composites.…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…However, stochastic load may occur during cyclic-fatigue loading, and cause extra damage in the composite, which affects the values of FLS. 27,28 Wu et al 29 performed experimental investigation on the vibration fatigue behavior of C/SiC composites under random loading. The stochastic vibration overloading degraded the fatigue life and FLS of the composites.…”
Section: Introductionmentioning
confidence: 99%
“…obtained the FLS of 2.5D‐C/SiC composites in warp and weft direction, that is, about 85% of the composite's tensile strength at room temperature. However, stochastic load may occur during cyclic‐fatigue loading, and cause extra damage in the composite, which affects the values of FLS 27,28 . Wu et al 29 .…”
Section: Introductionmentioning
confidence: 99%
“…During real application, random loading may occur and affect the fatigue life of composite. 25,26 Suzuki et al 27 developed a stiffness degradation model for life prediction of fiber-reinforced composites under stochastic loading. Gholami et al 28 predicted the fatigue life in laminated composites using a continuum damage mechanics-based model.…”
Section: Introductionmentioning
confidence: 99%
“…The paper reported by Paul Van Der Sypt et al reposes an experimental protocol on both micro and macroscopic level to monitor the mechanical response of a pin-loaded Carbon reinforced fiber polymer laminate under different cyclic loadings conditions [6]. Zengewn Wu et al studied that the fiber pull-out and fiber splitting were the majority failure mode of fibers in both the longitudinal and transverse directions and also damage in specimen is mainly due to the tensile force induced in reverse bending load [7]. Failure is observed around an open hole where stress is concentrated in mid of plies quasi-isotropic GFRP laminate under fatigue loading when dynamic strain reaches or exceeds static strain by Pintu Kumar Vishwakarma et al [8].…”
Section: Introductionmentioning
confidence: 99%