2 research outputs found
Bulk Fabrication of WS<sub>2</sub> Nanoplates: Investigation on the Morphology Evolution and Electrochemical Performance
Two-dimensional layered chalcogenide
WS<sub>2</sub>, similar to graphene, is considered to be very interesting
for materials scientists. However, to make it a useful material platform,
it is necessary to develop sophisticated synthesis methods to control
its morphology. In this paper, we present a simple approach to prepare
various morphologies of WS<sub>2</sub> nanostructures by direct thermal
evaporation of WO<sub>3</sub> and S powders onto Si substrates sputtered
with W film without using any nanostructured W-contained precursors
and highly toxic sulfide gases. This method can produce bulk quantities
of pure hexagonal, horizontally grown WS<sub>2</sub> nanoplates, vertically
grown nanoplates, and nanoplate-formed flowers simply by tuning the
distance between the substrate and source powders. The synthesis mechanism
and morphology evolution model were proposed. Moreover, when employed
as a thin-film anode material, the Li-ion battery with as-prepared,
vertically grown WS<sub>2</sub> nanoplates presented a rechargeable
performance between 3 and 0.01 V with a discharge capacity of about
773 mAh/cm<sup>3</sup> after recycling three times, much better than
its already-reported counterparts with randomly distributed WS<sub>2</sub> nanosheet electrodes, but the battery with horizontally grown
WS<sub>2</sub> nanoplates could not show any charge–discharge
cycling property, which could be attributed to the different structures
of WS<sub>2</sub> anodes for Li<sup>+</sup> ion intercalation or deintercalation
Densities and Viscosities for the Ternary Mixtures of <i>n</i>‑Undecane (1) + Butylcyclohexane (2) + 1‑Pentanol (3) and Corresponding Binaries at <i>T</i> = (293.15 to 333.15) K
The
actual composition is known to be highly responsible for the
physical and chemical properties of a fuel. To understand the foundational
physical properties of an aviation kerosene substitute mixture for
hypersonic aircraft, n-undecane, butylcyclohexane,
and 1-pentanol were used to construct a ternary system. The values
of density (ρ) and viscosity (η) for the ternary system
and three corresponding binaries were measured at temperatures T = (293.15 to 333.15) K and pressure p = 0.1 MPa. The Redlich–Kister equation was used to fit the
excess molar volumes (VmE) and viscosity deviations (Δη)
of the binary systems, while those of the ternary system were correlated
with four semi-empirical formulas (Cibulka, Singh, Redlich–Kister,
and Nagata–Tamura equations). The experimental results show
that the VmE values of the three binary mixtures have a
positive relationship with the mole fraction of nonpolar components,
while Δη values have a negative relationship. The non-ideal
behavior of mixtures is discussed from the perspective of molecular
interactions and structural effects. This work provides data support
and guidance for fuel compatibility research
