2021
DOI: 10.1002/app.50683
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Enhanced interlaminar shear and impact performance of woven carbon/epoxy composites interleaved with needle punched high performance polyethylene fiber nonwoven

Abstract: In this study, high-performance polyethylene (HPPE) fiber-based needle punched nonwovens were interleaved in cross-plied woven carbon fabric/epoxy composite laminates to enhance their interlaminar and impact properties. The placement of needle punched nonwoven interleaves exhibited considerable enhancement in interlaminar shear strength (ILSS), impact damage tolerance, and compression after impact (CAI) strength of laminates as evidenced by higher interlaminar strength, less absorbed energy, higher elastic ene… Show more

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Cited by 8 publications
(2 citation statements)
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References 54 publications
(90 reference statements)
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“…During CAI loading on continuous fiber reinforced composite material, the buckling of fiber, fiber‐matrix debonding and subsequent propagation of delamination caused by early pre‐impact damage may be accountable for composite failure. [ 39 ] Because of having wavy placement of filaments (up and down interlacement of longitudinal and horizontal filaments) in woven carbon fabric, the manufactured carbon/epoxy composite is more susceptible to fiber buckling. [ 40 ] The inclusion of PEEK particles in matrix may result in the formation of micro composites that resist micro buckling of the fiber.…”
Section: Resultsmentioning
confidence: 99%
“…During CAI loading on continuous fiber reinforced composite material, the buckling of fiber, fiber‐matrix debonding and subsequent propagation of delamination caused by early pre‐impact damage may be accountable for composite failure. [ 39 ] Because of having wavy placement of filaments (up and down interlacement of longitudinal and horizontal filaments) in woven carbon fabric, the manufactured carbon/epoxy composite is more susceptible to fiber buckling. [ 40 ] The inclusion of PEEK particles in matrix may result in the formation of micro composites that resist micro buckling of the fiber.…”
Section: Resultsmentioning
confidence: 99%
“…Firstly, the felt/felt layered needled structure, [8][9][10] which has a low volume density and weak in-plane mechanical properties, is mainly used as an anti-thermal insulation material; second, the felt/ base cloth layered needled structure. [11][12][13] Using unidirectional cloth, 12,14 woven cloth, 15 or braided cloth 16 as the base cloth, which has better in-plane performance and is commonly used in structural components such as brake disc materials, engine nozzles, throats, 17,18 and so forth. Recently, Yao et al 19,20 proposed a new needled structure and composite without felt that used half-cut cloth instead of felt, presented excellent interlaminar and in-plane performance, and was expected to be used as a material for high-speed aircraft radome covers.…”
Section: Introductionmentioning
confidence: 99%