2022
DOI: 10.1177/00219983211061823
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Numerical investigation of the dynamic behavior of a Ti/TiB functionally graded material using Split Hopkinson Pressure Bar test

Abstract: This work focuses on the mechanical behavior, at high strain rates, of metal-ceramic functionally graded materials (FGMs) using a Split Hopkinson Pressure Bar (SHPB) technique. The validity and the accuracy of the SHPB test results for these composite materials have not been meticulously studied due to their complex mechanical response under dynamic loadings. In this paper, numerical simulations of SHPB tests were performed to determine the dynamic response of specific FGMs at various strain rates. The effects… Show more

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Cited by 7 publications
(2 citation statements)
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“…There has been much research into the fabrication and characterization of functional gradient metal and ceramic composites. [19][20][21][22][23] The functional gradient structure concept has been applied to polymer matrix composites. Glass, 24 silicon carbide, 25,26 carbon fiber, [26][27][28] and other polymers such as polyurethane 29 have been used to make functionally graded epoxy-based composites.…”
Section: Introductionmentioning
confidence: 99%
“…There has been much research into the fabrication and characterization of functional gradient metal and ceramic composites. [19][20][21][22][23] The functional gradient structure concept has been applied to polymer matrix composites. Glass, 24 silicon carbide, 25,26 carbon fiber, [26][27][28] and other polymers such as polyurethane 29 have been used to make functionally graded epoxy-based composites.…”
Section: Introductionmentioning
confidence: 99%
“…Besides the quasi-static compression tests, the dynamic responses are also different between them [9]. As for composites or laminated materials, it is essential to understand their mechanical behavior and constitutive model under wide strain rate loading [10,11]. Zhang et al [12] employed bumpers constructed from Impedance-graded materials (IGM) to improve meteoroid/debris shielding structures for spacecrafts.…”
Section: Introductionmentioning
confidence: 99%