| 000 | 02387nam a2200265Ia 4500 | ||
|---|---|---|---|
| 003 | MX-MdCICY | ||
| 005 | 20250625164353.0 | ||
| 040 | _cCICY | ||
| 090 | _aB-21347 | ||
| 245 | 1 | 0 | _aExtreme strain rate deformation of nacre-inspired graphene/copper nanocomposites under laser-induced hypersonic micro-projectile impact |
| 490 | 0 | _aComposites Part B: Engineering. 235, 109763, 2022, DOI: 10.1016/j.compositesb.2022.109763 | |
| 520 | 3 | _aDesign and fabrication of impact resistant metal materials under extreme strain rate conditions is of great importance, especially in the field of collision protection of satellites and spacecraft. As inspired by the 'brick-and-mortar' microstructure induced excellent impact resistance in natural nacre, coupling with extraordinary intrinsic impact resistance of graphene (Gr), in this work a nacre-inspired Gr/Cu nanocomposite is fabricated, and its anisotropic extreme strain rate (at a level of ?108/s) deformation behaviors are studied by using laser-induced microprojectile impact tests (up to a speed of ?2.5 Km/s). Such extreme impact loading together with pinning effect of graphene can lead to highly stabilized high-density deformation twins and stacking faults at impact front even in the ultrafine grained Cu matrix. As the loading direction perpendicular to the composite layers, volume of severely-deformed region and the density of twinning and stacking faults at impact front is one third and half of that in the parallel impact direction, respectively. Such discrepancies indicate the capacity to dissipate impact energy in the perpendicular direction is ?6 times higher than that of the parallel one, in spite of only ?0.9 vol% graphene incorporated in the bio-inspired composites, evidencing architecture design plays an important role in impact resistance of materials under extreme dynamic conditions. © 2022 Elsevier Ltd | |
| 650 | 1 | 4 | _aCOPPER |
| 650 | 1 | 4 | _aEXTREME STRAIN RATE DEFORMATION |
| 650 | 1 | 4 | _aGRAPHENE |
| 650 | 1 | 4 | _aLASER-INDUCED IMPACTS |
| 650 | 1 | 4 | _aMETAL MATRIX COMPOSITES |
| 700 | 1 | 2 | _aPeng Y. |
| 700 | 1 | 2 | _aLuo G. |
| 700 | 1 | 2 | _aHu Y. |
| 700 | 1 | 2 | _aXiong D.-B. |
| 856 | 4 | 0 |
_uhttps://drive.google.com/file/d/1uO8JG9aIXsapOiuxmxFS7IwD7l9malsW/view?usp=drivesdk _zPara ver el documento ingresa a Google con tu cuenta @cicy.edu.mx |
| 942 |
_2Loc _cREF1 |
||
| 008 | 250602s9999 xx |||||s2 |||| ||und|d | ||
| 999 |
_c55411 _d55411 |
||