2017
DOI: 10.1080/21663831.2017.1386241
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Grain boundary-assisted deformation in graphene–Al nanolaminated composite micro-pillars

Abstract: Micro-pillars with diameters varying from 0.5 to 3.5 µm were fabricated from bulk nanolaminated graphene (in the form of reduced grapheme oxide, RGO)-Al composite. Upon uniaxial compression, the pillar strengths exhibited no obvious size effect, and the pillars of larger diameters possessed smoother stress-strain response, as opposed to the jerky deformation of their smaller counterparts. A corresponding transition in the deformation mode from Al layer extrusion to shear fracture over decreasing pillar diamete… Show more

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Cited by 27 publications
(6 citation statements)
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“…HS materials have very diverse microstructures [1], including heterogeneous lamella structure [2], gradient structure [3][4][5][6][7][8], laminate structure [9,10], dual phase CONTACT Yuntian Zhu ytzhu@ncsu.edu; Xiaolei Wu xlwu@imech.ac.cn structure [11][12][13], harmonic structure [14][15][16], bi-modal structure [17][18][19][20], metal matrix composites [21][22][23][24][25][26], etc. These apparently very diverse structures have a common feature: all of them consist of both soft domains and hard domains with dramatically different flow stresses (or strength) [1].…”
Section: Introductionmentioning
confidence: 99%
“…HS materials have very diverse microstructures [1], including heterogeneous lamella structure [2], gradient structure [3][4][5][6][7][8], laminate structure [9,10], dual phase CONTACT Yuntian Zhu ytzhu@ncsu.edu; Xiaolei Wu xlwu@imech.ac.cn structure [11][12][13], harmonic structure [14][15][16], bi-modal structure [17][18][19][20], metal matrix composites [21][22][23][24][25][26], etc. These apparently very diverse structures have a common feature: all of them consist of both soft domains and hard domains with dramatically different flow stresses (or strength) [1].…”
Section: Introductionmentioning
confidence: 99%
“…flow (6) where M is the Taylor factor, b is the length of the Burgers vector of perfect dislocations in Cu, h′ is the layer thickness parallel with the sliding plane, h is the thickness of individual single-layer Cu, with h = h′ sin 71.2°, ν is the Poisson's ratio of Cu, f is the characteristic interface stress, μ* is the mean shear modulus, α is the core cutoff parameter, and L is the mean shear spacing of the sliding array (L = b/ε). Considering that in the plastic flow stage, Shockley partial dislocations dominates plastic deformation, we replace b with b p , i.e., the length of the Burgers vector of the partial dislocations in Cu, and rewrite eq 6 as…”
Section: ■ Results and Discussionmentioning
confidence: 99%
“…Traditional reinforcement constituents are usually hard materials with higher strength, such as silicon carbide, aluminum oxide, and titanium carbide . In recent years, nanocarbon materials have also been considered because of their excellent mechanical and physical properties, among which graphene (Gr) is one of the most promising representatives because of its ultrahigh intrinsic strength (∼130 GPa) and Young’s modulus (1000 GPa). …”
Section: Introductionmentioning
confidence: 99%
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“…5,[12][13][14][15][16][17][18][19][20][21][22][23] However, the flow stress of nano-twinned metals was found to decrease right after yielding, showing rather limited work hardening ability. 17,[24][25][26] Alternatively, inspired by the concept of "grain boundary engineering" that could improve the work hardening ability of metallic composites, [27][28][29][30][31][32][33][34][35] graphene that processed ultrahigh Young's modulus and tensile strength [36][37][38][39][40][41][42] was applied not only to be the reinforced phase but also to introduce metal/graphene interfaces thus may enhance the mechanical properties of the composites.…”
Section: Introductionmentioning
confidence: 99%