133 research outputs found
The effect of interstitial clusters and vacancies on the STM image of graphite
Making use of the tight-binding Green's function technique, we have
calculated the STM images of graphite with surface and sub-surface defects,
while taking into account the relaxation of the lattice due to defects. We have
demonstrated that two different physical mechanisms may result in the formation
of hillocks in the STM images: buckling of the graphite surface due to
interstitials between the uppermost graphite layers and the enhancement of the
electron density of states close to the Fermi energy on the carbon atoms in the
vicinity of vacancies. Our results indicate that small hillocks may originate
both from the interstitial clusters and from the vacancies. By contrast,
however, large hillocks in excess of 10 \AA~ in diameter can be caused only by
interstitial clusters.Comment: Submitted to Surface Scienc
Clusters of interstitial carbon atoms near the graphite surface as a possible origin of dome-like features observed by STM
Formation of clusters of interstitial carbon atoms between the surface and
second atomic layers of graphite is demonstrated by means of molecular dynamics
simulations. It is shown that interstitial clusters result in the dome-like
surface features that may be associated with some of the hillocks observed by
STM on the irradiated graphite surface.Comment: 7 pages, 7 eps figures, submitted to Surface Scienc
Electron Wave Function in Armchair Graphene Nanoribbons
By using analytical solution of a tight-binding model for armchair
nanoribbons, it is confirmed that the solution represents the standing wave
formed by intervalley scattering and that pseudospin is invariant under the
scattering. The phase space of armchair nanoribbon which includes a single
Dirac singularity is specified. By examining the effects of boundary
perturbations on the wave function, we suggest that the existance of a strong
boundary potential is inconsistent with the observation in a recent scanning
tunneling microscopy. Some of the possible electron-density superstructure
patterns near a step armchair edge located on top of graphite are presented. It
is demonstrated that a selection rule for the G band in Raman spectroscopy can
be most easily reproduced with the analytical solution.Comment: 7 pages, 4 figure
Study of Au/n- ZnSe contact by ballistic electron emission microscopy
Ballistic Electron Emission Microscopy (BEEM) has been used to characterise the Au/n-ZnSe contact. A mean statistical BEEM threshold of 1.63eV is in good agreement with literature. Metal - Insulator- Semiconductor (MIS) structures are invoked to explain the Schottky barrier height dispersion and the observed shift of BEEM thresholds to higher values.Ballistic Electron Emission Microscopy (BEEM) has been used to characterise the Au/n-ZnSe contact. A mean statistical BEEM threshold of 1.63eV is in good agreement with literature. Metal - Insulator- Semiconductor (MIS) structures are invoked to explain the Schottky barrier height dispersion and the observed shift of BEEM thresholds to higher values
u/n-Si(100) contact homogeneity studied by direct and reverse ballistic electron emission microscopy and spectroscopy
The Au/n-Si(100) contact has been studied using reverse ballistic electron emission microscopy and spectroscopy. Two types of localised collector currents have been observed; one, positive corresponding to electron injection into Si, and the other, negative, associated with hole injection into the semiconductor. The comparative trial of BEEM and reverse BEEM images from the same area shows this difference to be linked to the interface structure. Effects of surface roughness on the observed contrasts are also discussed.The Au/n-Si(100) contact has been studied using reverse ballistic electron emission microscopy and spectroscopy. Two types of localised collector currents have been observed; one, positive corresponding to electron injection into Si, and the other, negative, associated with hole injection into the semiconductor. The comparative trial of BEEM and reverse BEEM images from the same area shows this difference to be linked to the interface structure. Effects of surface roughness on the observed contrasts are also discussed
Etude par Microscopie a Effet Tunnel de surfaces de graphite implante et autres applications
SIGLEINIST T 76530 / INIST-CNRS - Institut de l'Information Scientifique et TechniqueFRFranc
Scanning Tunneling Microscopy Observation of Damage on HOPG Surface Induced by H+ and other Light Ions**Supported by National Natural Science Foundation of China
Méthode de Boltzmann sur réseaux hybride : application aux écoulements compressibles complexes
Les travaux présentés dans ce manuscrit s'inscrivent dans une démarche de modélisation des systèmes physiques et décrivent une méthode numérique innovante pour la résolution des équations de conservation relatives à la mécanique des fluides dans le cas des écoulements compressibles. La méthode de Boltzmann sur réseaux est introduite en tant qu'outil de modélisation limité aux écoulements incompressibles. Pour répondre à cette problématique, une dérivation rigoureuse d'un modèle compressible hybride n'incluant que les plus proches voisins est présentée. Ce modèle est ensuite testé sur plusieurs applications présentant une complexité croissante grâce à l'ajout d'ingrédients numériques. La mise en place de conditions aux limites, d'une méthode capture des chocs, de raffinements de maillages et d'un modèle de turbulence ont ainsi permis la simulation d'une aile Onera M6 entourée par un écoulement compressible et turbulent. Basé sur les caractéristiques du système d'Euler et sur un couplage fort avec les flux numériques de masse et de quantité de mouvement issus de la méthode de Boltzmann sur réseaux, un schéma conservatif pour l'équation d'énergie est dérivé. Ce travail se termine par une étude du traitement des conditions aux limites liées à la méthode compressible. Les défauts de la méthode d'interpolation des variables macroscopiques sur les nœuds proches des parois initialement proposée sont mis en avant et certaines pistes d'amélioration sont proposéesThe work presented in this manuscript is part of an approach to modeling physical systems and describes an innovative numerical method for solving fluid mechanics conservation equations in the scope of compressible flows. The Lattice Boltzmann method is presented as a modeling tool that is restricted to incompressible flows. To address this issue, a rigorous derivation of a hybrid compressible model that includes only the nearest neighbors is presented. This model is then tested on a variety of applications with increasing complexity as numerical ingredients are added. With the addition of boundary conditions, a shock-capturing method, mesh refinements, and a turbulence model, the simulation of a Onera M6 wing surrounded by a compressible and turbulent flow was possible. A conservative scheme for the energy equation is derived based on the characteristics of the Euler system and a strong coupling with the fluxs of mass and momentum derived from the Lattice Boltzmann method. The study of compressible boundary conditions concludes this work. The shortcomings of the initially proposed method of interpolating macroscopic variables on nodes close to walls are highlighted, and some areas for improvement are suggeste
STUDY OF A PRESSURE-BASED HYBRID LATTICE BOLTZMANN METHOD FOR THE SIMULATION OF COMPRESSIBLE FLOWS
International audienceThe Lattice Boltzmann Method (LBM) is an alternative technique for the simulation and mod-elling of fluid flows based on the Boltzmann equation. One of its advantages is its ability tohandle very complex geometries with massively parallel computing. The LBM has achieved greatsuccess in simulating nearly incompressible and isothermal fluid flows, but it restricts its appli-cation range. A particularly active topic of investigation is its extension to more complex flows(e.g. multi-phase, thermal, compressible). We propose a pressure-based prediction-correction hybrid LBM model compatible with nearest-neighbor lattices (D2Q9 and D3Q19) with asingle time relaxation process, to simulate subsonic and transonic compressible flows withoutshock.The approach is hybrid: mass and momentum conservation equations are computed usinga LBM solver while an entropy conservation equation is solved via a finite difference approach.Following, an adequate forcing term is added to reproduce a correct viscous stress tensorand hybrid recursive regularized approach is used to stabilize the solution. Discretization ofthe entropy equation with viscous heat dissipation, in the finite difference part of the solver, isstudied to improve accuracy of the scheme and to reduce the cost of calculations.Validation of this new method is carried out on a number of canonical cases, systematicallychallenging the coupling between velocity, pressure and temperature, including pressure wavepropagation, and thermal Couette flows
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