1-2/2009
Contents:
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A.Wilk, M.Skuta, Laboratory Tests of the Aerodynamic Drag Coefficient of the Flag as a Body
with Low Stiffness
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H.Kudela, Z.M.Malecha, Viscous Flow Modeling Using the Vortex Particles Method
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B.Zhou, B.You, W.Wu, K-Q.Wu, Leading Edge Skewed-Swept Diagonal Compressor Rotor and Numerical Analysis on Its
Internal Flow Mechanism
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K.Murawski, Godunov-Type Numerical Methods for One- and Two-Component Magnetohydrodynamic Equations
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| full text
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M.Gruszecki, K.Murawski, Numerical Methods for Fast Magnetoacoustic Waves in Solar Coronal Loops
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| full text
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A.Dawid, K.Gorny, Dynamics of Endohedral Fullerene K+@C60 Inside Single Walled
Carbon Nanotube: MD Simulation
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Z.Dendzik, D.Chrobak, R.Nowak, Elastic Constants and Analytic Bond Order Potential for Atomistic Simulations
of Simple Cubic Tungsten Trioxide
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| full text
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S.Olszewski, T.Rolinski, New Kind of Parameterization Applied to the Fermi Surface of a Crystalline Solid.
Part I: Electron Observables and Curvature Parameters Examined on the Surface
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| full text
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T.Rolinski, S.Olszewski, New Kind of Parameterization Applied to the Fermi Surface of a Crystalline Solid.
Part II: Density of States and Lengths of Arcs Calculated as a Check of the Theory
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| full text
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S.Leble, W.Pelc, Analytic-Numerical Model of a Convective Boundary Layer and Heat Transfer
on a Horizontal Cone
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Y.Chaplya, S.Kondrat, O.Hrytsyna, V.Kondrat, On Electromechanical Phenomena in Thin Dielectric Films
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A.Contento, A.Di Egidio, J.Dziedzic, A.Tatone, Modeling the Contact of Stiff and Soft Bodies with a Rigid Support by Short Range Force
Fields
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| full text
Abstracts:
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A.Wilk, M.Skuta, Laboratory Tests of the Aerodynamic Drag Coefficient of the Flag as a Body
with Low Stiffness
The shape and drag of bodies with small stiffness may change during the airflow. This
problem refers to such bodies as flags, bands, banners, flapping sails as well as blades
and cables which vibrate due to the flow.
Laboratory tests carried out to point out the aerodynamic drag coefficient of a flag
are discussed in this article. The laboratory tests were carried out in an aerodynamic
tunnel at different airflow velocities for flags with different dimensions made of
fabrics of different roughness and stiffness. The drag coefficient value decreases with
the increasing airflow velocity. The drag coefficient is higher for materials with
higher roughness. The drag coefficient value is also influenced by the fabric stiffness
and kind of edge.
Great engineering importance to the stability of a structure (e.g. a flag mast) and
the safety of nearby persons and buildings are attached to the analysed problem.
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H.Kudela, Z.M.Malecha, Viscous Flow Modeling Using the Vortex Particles Method
The vortex particle method is an easy and attractive tool to analyze flow phenomena by
investigating vorticity fields and the generation of vorticity at solid walls. The
vorticity generation at the walls and its introduction to the flow is of fundamental
significance for understanding such phenomena as transition to turbulence, boundary layer
separation in an eruptive way, and vortex structures regeneration. In the present study
the vortex-in-cell usefulness of the method has been tested using a variety of simple
test problems: the Poiseuille flow, the second Stokes problem, the cavity, the backward
step flow, the vortex dipole interaction with the wall, and the flow past a square
cylinder in the vicinity of a wall in order to illustrate the correctness and usefulness
of the vortex particle method.
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B.Zhou, B.You, W.Wu, K-Q.Wu, Leading Edge Skewed-Swept Diagonal Compressor Rotor and Numerical Analysis on Its
Internal Flow Mechanism
The structure of each part of a diagonal compressor directly affects its overall
performance and internal flow. We introduce the Reynolds-averaged Navier-Stokes flow
simulation for unit calculation on the whole system including a diagonal impeller, a
vaneless diffuser and a volute. By analyzing different flow chromatograms of specific
sections, we can compare the configuration of three types of diffusers and volutes and
the meridian flow status of the corresponding diagonal compressors which serves as a
basis for the impeller flow path as well as for its matching designs. Considering the
interference between the rotor and the upstream and downstream stillness body, this
thesis analyzes how the vaneless diffuser meridian flow path, the volute flow path and
its section secondary flow affect the upstream rotor flow. Both the calculation and
experimental data on the rotor outlet are compared, as well as the calculated numerical
value of the meridian plane streamline distribution and the diffuser velocity
distribution, upstream and downstream, coincides with the designed numerical value.
Without changing the conventional quasi-three-dimensional design system, the thesis
applies the annulus wall boundary layer theory and the velocity distribution diagram to
sweep and skew the leading edge of the airfoil. A performance test shows that the leading
edge skewed-swept diagonal rotor can better improve the stall characteristic in a low
flow rate area and expand the surge margin, compared with conventional diagonal rotor. It
can also efficiently restrain the low-momentum fluid conglomeration near the wall region
and reduce the secondary flow loss by sweeping and skewing the blade properly. The
purpose of the thesis is to make a contribution to optimizing the overall structure
design of diagonal compressors and to study further the complex internal flow between the
leading edge skewed-swept diagonal rotor and the cover.
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K.Murawski, Godunov-Type Numerical Methods for One- and Two-Component Magnetohydrodynamic Equations
In this paper we review Godunov-type numerical methods for one- and two-component
magnetohydrodynamic equations. Solving these equations numerically is a formidable task
as a result of the internal complexity of these equations and the requirements of
∇⋅B=0. We present several results of advanced numerical simulations for
complex systems. These results prove that the numerical codes which are based on
Godunov-type methods, cope with all problems very well.
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M.Gruszecki, K.Murawski, Numerical Methods for Fast Magnetoacoustic Waves in Solar Coronal Loops
Numerical methods for standing fast magnetoacoustic kink waves in an isothermal solar
coronal slab with a field aligned flow are considered. Such waves are triggered
impulsively by a velocity pulse that is initially launched in an ambient medium. The
spatial and temporal signatures of these waves are determined by solving two-dimensional,
ideal magnetohydrodynamic equations numerically. The Ramses code which resolves complex
spatial structures by adopting an adaptive mesh refinement technique and shock-capturing
capabilities is used. The numerical results show that spatial and temporal wave
signatures are reminiscent to the recent observational findings.
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A.Dawid, K.Gorny, Dynamics of Endohedral Fullerene K+@C60 Inside Single Walled
Carbon Nanotube: MD Simulation
K+@C60 endohedral fullerenes inside armchair, zigzag and chiral
nanotubes were simulated using the MD technique. The structure of the endohedral
fullerene sample was estimated by calculating the radial distribution function. The
angular and translational velocity autocorrelation functions and their Fourier transforms
were also calculated. The frequency dependence of potassium ion vibrations in different
nanotubes at room temperature was observed and discussed. A dependency between the
angular motion of endo-fullerenes and the nanotube chirality was found.
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Z.Dendzik, D.Chrobak, R.Nowak, Elastic Constants and Analytic Bond Order Potential for Atomistic Simulations
of Simple Cubic Tungsten Trioxide
A set of elastic constants was calculated and a parametrization of the potential was
derived for simple cubic tungsten trioxide based on an analytical bond-order scheme. It
was shown that the obtained parametrization provided a good description of interatomic
forces and such properties as the lattice constant, the bulk modulus and the elastic
constants.
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S.Olszewski, T.Rolinski, New Kind of Parameterization Applied to the Fermi Surface of a Crystalline Solid.
Part I: Electron Observables and Curvature Parameters Examined on the Surface
A magnetic field applied to a crystalline solid causes the electron states on the Fermi
surface to circulate along the orbits located on the planes normal to the applied field.
For a sufficiently weak field the separate orbits can cover the whole closed Fermi
surface. A suitable parameterization of the states on the orbits should be done in a
different way than a conventional parameterization applied for the electron states by
Bloch. This new kind of parameterization becomes quite simple when the magnetic field is
assumed to be directed parallel to one of the crystallographic axes. Computationally, a
new description of the electron states on the Fermi surface becomes on many occasions
more flexible in its use than the Bloch’s one. The simplifications concern mainly an
examination of the curvature parameters of the Fermi surface and extremal properties of
the electron observables, for example that of electron velocity. Solely the states in the
cubic crystal lattices were considered as examples.
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T.Rolinski, S.Olszewski, New Kind of Parameterization Applied to the Fermi Surface of a Crystalline Solid.
Part II: Density of States and Lengths of Arcs Calculated as a Check of the Theory
In order to check the validity of parameterization of electron states on the Fermi
surface developed in the preceding paper, this parameterization is applied to the
calculation of some definite crystal properties. The first property is the density of
electron states versus energy in simple cubic and body-centered cubic crystal lattices,
examined formerly on the basis of the Bloch parameterization of electron states by
Jelitto; the other property is the length of some special arcs extended on the surfaces.
The parameterizations of both approaches, that of the present paper and that developed on
the basis of the Bloch states, are found to give results remaining in remarkable
agreement.
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S.Leble, W.Pelc, Analytic-Numerical Model of a Convective Boundary Layer and Heat Transfer
on a Horizontal Cone
An approximate analytical solution of a two dimensional problem for stationary
Navier-Stokes, continuity and Fourier-Kirchhoff equations describing a free convective
heat transfer from an isothermal cone is presented. The problem formulation is based on
assumptions typical for natural convection: non-compressibility and the Boussinesq
approximation. The solution is based on Frobenius expansions at the vicinities of two
points: the initial point and the singular point of the boundary layer equation.
Numerical matching of the expansions and Nusselt number evaluations are traced.
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Y.Chaplya, S.Kondrat, O.Hrytsyna, V.Kondrat, On Electromechanical Phenomena in Thin Dielectric Films
A model of electro-magneto-thermo-mechanics for electroconducting polarized
nonferromagnetic medium is proposed which takes into account the local mass displacement
in addition to the local electric charge displacement. The corresponding key set of
equations is written. Using the isothermal approximation, the model is applied to
describe the interface inhomogeneity of a stressed state, the polarization and coupled
electric charge in thin dielectric films. An anomalous dependence of the electric
capacity on the thickness of a thin dielectric film, observed experimentally by Mead, is
also studied and is shown to be well captured by the present approach.
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A.Contento, A.Di Egidio, J.Dziedzic, A.Tatone, Modeling the Contact of Stiff and Soft Bodies with a Rigid Support by Short Range Force
Fields
Body impact-contact dynamics is a classical subject in mechanics. Most of the papers on
the subject are based on a kinematical or impulse-exchange approach. In this paper a
different approach has been adopted. It consists in assigning a constitutive description
for the contact forces between the boundaries of bodies which get close to each other. In
particular, a field of short range forces has been used to model the interaction between
an affine body and the planar surface of a fixed rigid support. These forces are able to
describe the impact, friction and adhesion allowing the body to have complex motions
which look rather realistic. By an affine body we mean a body which undergoes affine, or
homogeneous, deformations. Depending on the material, such a body can show very different
behavior, from a quite rigid motion to a motion characterized by very large deformations.
A soft body is assumed to be made of a viscous incompressible Mooney-Rivlin material.
Though a microscopic model of surface interaction could be used in a multiscale approach,
the description provided here is macroscopic only.
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