Effect of Al and Cd sacrificial coatings on the wear of steel substrates

Behera, P.; Chromik, Richard R.; Yue, Stephen

doi:10.1016/j.wear.2021.203847

Cited by 5 publications

(1 citation statement)

References 37 publications

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“…However, due to their anisotropy, their out-of-plane properties are poor; they become susceptible to delamination (one of the lower energy failure modes), and possess poor interlaminar strength and fatigue resistance for structural applications. [1][2][3][4][5][6][7][8][9] The issue of delamination is of primary concern in FRP composite structures subjected to fatigue loads such as tidal turbine blades and wind blades. The study of the performance of static and fatigue loading of delamination is a thrust area and has been numerous articles in present years.…”

Section: Introductionmentioning

confidence: 99%

Mode I and II interlaminar fracture toughness of glass/carbon inter‐ply hybrid FRP composites: Effects of stacking sequence and testing temperature

et al. 2023

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Even though laminated FRP composites show exceptional performance in various modes of loading, they are susceptible to delamination. The ambient temperature and elevated temperature delamination resistance of glass/carbon fiber interply hybrid composites were assessed via mode I and mode II interlaminar fracture toughness tests performed at 30, 50 and 70 C. Interply hybrid composites performed better than composites with single type of fiber. The fracture toughness of inter-ply hybrid composites varied with the stacking position. At 30 C, mode I fracture toughness value of alternative glass and carbon fiber stacking sequence (G 1 C 1 ) 5 of hybrid composite showed 40% improvement over 10 layered carbon/epoxy (C 10 ) composite. Further, Mode II fracture toughness of C 5 G 5 composite showed 22% enhancement, and C 10 exhibited 42% improvement over 10-layered glass/epoxy composite. Increasing the test temperature of all composites improved their G IC and G IIC values. The increment in the mode I fracture toughness properties of all composite was in the range of 5%-23% at 70 C from its room temperature value. The fractographic images of fractured samples were studied under a scanning electron microscope and failure mechanisms of composites were identified. K E Y W O R D Shigh temperature durability, inter-ply hybrid composite, mode I ILFT, mode II ILFT, stacking sequence of glass and carbon fibers

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