2015
DOI: 10.1016/j.ijimpeng.2015.08.014
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Hybridized composite architecture for mitigation of non-penetrating ballistic trauma

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Cited by 33 publications
(16 citation statements)
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“…Where E, ρ, σ, and Ɛ are the Young"s modulus, density, tensile strength, and tensile failure strain of the fibre. This analysis however does not consider several effects such as the matrix properties [13], the influence of fibre orientation [14], and strain rate dependency of the fibres [8]. It has recently been shown that the layup orientation can have a large effect on not only the velocity to 50% chance of perforation (V50), but also in limiting back face deflection (BFD) [14][15].…”
Section: Accepted Manuscriptmentioning
confidence: 99%
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“…Where E, ρ, σ, and Ɛ are the Young"s modulus, density, tensile strength, and tensile failure strain of the fibre. This analysis however does not consider several effects such as the matrix properties [13], the influence of fibre orientation [14], and strain rate dependency of the fibres [8]. It has recently been shown that the layup orientation can have a large effect on not only the velocity to 50% chance of perforation (V50), but also in limiting back face deflection (BFD) [14][15].…”
Section: Accepted Manuscriptmentioning
confidence: 99%
“…This analysis however does not consider several effects such as the matrix properties [13], the influence of fibre orientation [14], and strain rate dependency of the fibres [8]. It has recently been shown that the layup orientation can have a large effect on not only the velocity to 50% chance of perforation (V50), but also in limiting back face deflection (BFD) [14][15]. Reducing BFD for an impact that does not cause laminate perforation is particularly important for applications such as helmets that have stringent design specifications to limit the amount of transverse deflection in order to prevent blunt trauma injuries.…”
Section: Accepted Manuscriptmentioning
confidence: 99%
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“…The figure demonstrated that compared with the molding temperature of 80 °C, v 50 , E t , and E D respectively increased by 5.88%, 12.60%, and 11.80% when the molding temperature reached 120 °C. It has been demonstrated that the increased coupling with the boundaries of the composites through interlaminar shear, membrane stretching, and fiber pull‐in govern the energy absorption during the progressive penetration event . With the increasing of molding temperature, the interlaminar shear strength gradually increases.…”
Section: Resultsmentioning
confidence: 99%
“…It has been demonstrated that the increased coupling with the boundaries of the composites through interlaminar shear, membrane stretching, and fiber pull-in govern the energy absorption during the progressive penetration event. 32 With the increasing of molding temperature, the interlaminar shear strength gradually increases. Therefore, it can be deduced that the kinetic energy of the projectile can be validly dissipated by the delamination of the laminate prepared under higher molding temperature.…”
Section: Effect Of Molding Temperature On Ballistic Performance Of Uhmentioning
confidence: 99%