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    F Kosel

    The development of a new composite that is compounded of natural fibres and of a low price polymer, such as HDPE or PP, began in the last decade of the past century. While this is a rather new material no attempts have been made to... more
    The development of a new composite that is compounded of natural fibres and of a low price polymer, such as HDPE or PP, began in the last decade of the past century. While this is a rather new material no attempts have been made to analytically describe and simulate mechanical properties of this material. There is also a great lack of knowledge in describing fine tuned processing parameters. Therefore, in the first part of this article micromechanical approach based upon Generalised Method of Cells (GMC) is introduced to simulate properties of injection moulded wood-plastic composite compounded of polypropylene (PP) or polystyrene (PS) and of wood or cellulose short fibres. Materials have first been scanned with an optical and electron microscope to determine average fibre properties and their scatter. These values are then used to determine elastic and plastic response of the composite alongside with its tensile strength and maximum elongation, where the Tsai-Hill failure criterion...
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    This paper presents the experimental and numerical results for the flow around a sphere at subcritical Reynolds number of 50 000. Two experimental techniques, the hot-wire and the laser-doppler anemometry (HWA and LDA), are used to obtain... more
    This paper presents the experimental and numerical results for the flow around a sphere at subcritical Reynolds number of 50 000. Two experimental techniques, the hot-wire and the laser-doppler anemometry (HWA and LDA), are used to obtain the mean velocity field and the turbulence quantities. These two experiments provided very similar results. Results of a large-eddy simulation (LES) and several Reynolds-averaged Navier-Stokes (RANS) equation models are compared to the experimental results. The LES results are in reasonable agreement with experiments while RANS underpredict the drag coefficient up to 50% compared to experiments and turbulence quantities were predicted far from the experimental values.
    This work analitically and experimentally investigates nonlinear snap-through of a simple class of elastic space trusses in the shape of a regular pyramid. Joints located at the vertices of the base polygon are pinned while the joint at... more
    This work analitically and experimentally investigates nonlinear snap-through of a simple class of elastic space trusses in the shape of a regular pyramid. Joints located at the vertices of the base polygon are pinned while the joint at the apex is subjected to a proportionally increasing load acting in the vertical direction. A pyramid truss model has been designed, machined and successfully tested in learning environments to facilitate understanding of the mechanics of truss structures, geometric nonlinearity and stability. Solutions are derived for each load condition under the common hypotheses of linear material law, small or moderate axial deformation in bars and large nodal displacements. For pyramidal truss we determined a function of force in dependence of vertical displacement of uniaxial structural elements for different starting angles at which the uniaxial structural elements were clamped. Accuracy of analytical solution for snap-through system, which we got for different starting angles of uniaxial structural elements, was verified on experimental results obtained in the laboratory.
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    ABSTRACT The bending behaviour of thin-walled profiles made from high-strength steels with respect to a changing angle of the bending plane or, in other words, the rotation of the section geometry on the longitudinal axis of the profile,... more
    ABSTRACT The bending behaviour of thin-walled profiles made from high-strength steels with respect to a changing angle of the bending plane or, in other words, the rotation of the section geometry on the longitudinal axis of the profile, has not yet been fully characterized. The investigations presented in this paper lead to an improvement of the description for bending square hollow sections under unified and constant loading conditions, and contribute to the general understanding of such bending problems. The methodological approach is based on analytic, numerical, and experimental analysis. The analytical formulation is primarily built on the principle of a simplified cantilever beam model. Bending curvatures are assumed to be generated with constant radiuses of curvatures. The change of the angle of the section, with respect to the direction of bending, is applied before bending and remains unchanged throughout the process. In this way, the effects of a changing angle with regard to the direction of bending are analyzed for several constant curvatures and angles of 2D bent profiles. With a clear understanding of the 2D bending of high strength profiles, the same principles can also be used incrementally for analyses of 3D bending. The analytical theory is tested with an emphasis on using profiles with high-strength material properties compared to profiles made from standard low-carbon steel, by using the innovative torque superposed spatial (TSS) bending method. The results are supported by FE models generated with the Abaqus numerical FEM tool and verified with the results of actual experiments.
    Fractures of the distal humerus are most commonly fixed by open reduction and internal fixation, using plates and screws, either in a locking or in a non-locking construct. Three different plating systems are commonly used in practice.... more
    Fractures of the distal humerus are most commonly fixed by open reduction and internal fixation, using plates and screws, either in a locking or in a non-locking construct. Three different plating systems are commonly used in practice. The most important differences between them are in plate orientation, which affects both the rigidity of the osteosynthesis and invasiveness of the surgical procedure. Unfortunately, there is no common agreement between surgeons about which plate configuration brings the best clinical outcome. In this study, we investigate the theoretical rigidity of plate osteosyntheses considering two types of AO/ASIF configurations (90° angle between plates), Mayo clinic (Acumed) configuration (180° between plates) and dorsal fixation of both plates. We also compared the results for cases with and without contact between the bone fragments. In the case of no bone contact, the Mayo clinic plate configuration is found to be the most rigid, followed by both AO/ASIF pl...
    ABSTRACT A digital image could be used as a source of data for various dimensional measurements. After acquiring the digital image of the measured object, the object contour is determined. The contour is composed of a sequence of distinct... more
    ABSTRACT A digital image could be used as a source of data for various dimensional measurements. After acquiring the digital image of the measured object, the object contour is determined. The contour is composed of a sequence of distinct pixels which contain centre points. This is a representation of a digital curve or digital arc from which the object length or the perimeter could be determined. In order to calculate the approximate length of the object, we introduce a new algorithm called an anchored discrete convolution. The algorithm is based on a discrete convolution by using different convolution masks and points anchored in the pixels. Unfortunately, the use of an ordinary convolution distorts the curve shape and introduces large errors in length calculation. In our case the anchoring limits the point shifting into the pixel area during the calculation of the curve length. In this paper different convolution masks are used on an experimental digital curve in order to evaluate the presented algorithm as a measuring tool. In addition, different real objects were optically scanned and the perimeters of the objects were determined from the acquired images. Keywords: anchored discrete convolution, digital image, length measurement.
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    The paper treats the thermoelastic problem of a shrink fit between an eccentric circular annulus and a shaft. At ambient temperature, prior to heating and assembly an eccentric annulus has an outer radius R, inner radius r1 but the... more
    The paper treats the thermoelastic problem of a shrink fit between an eccentric circular annulus and a shaft. At ambient temperature, prior to heating and assembly an eccentric annulus has an outer radius R, inner radius r1 but the shaft's radius is by a value δ'1 greater than radius r1. An eccentric annulus is homogeneously heated for a certain value
    ... Hančič Aleš 1,a , Kuzman Karl 2,b , Kosel Franc 2,c , Glojek Andrej 1,d , Cunha Antonio M. 3,e , Gantar Gašper 1,f 1TECOS ... The deformation input data are non-existent yet, so extensive search for correct parameters has begun.... more
    ... Hančič Aleš 1,a , Kuzman Karl 2,b , Kosel Franc 2,c , Glojek Andrej 1,d , Cunha Antonio M. 3,e , Gantar Gašper 1,f 1TECOS ... The deformation input data are non-existent yet, so extensive search for correct parameters has begun. Numerous ...
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    This article investigates a method for obtaining all equilibrium configurations of a cantilever beam subjected to an end load with a constant angle of inclination. The formulation is based on plane finite-strain beam theory in the elastic... more
    This article investigates a method for obtaining all equilibrium configurations of a cantilever beam subjected to an end load with a constant angle of inclination. The formulation is based on plane finite-strain beam theory in the elastic domain. An example of a cantilever beam subjected to a horizontal pressure force is discussed in detail.
    The paper deals with stresses, strains and buckling conditions in the thin axi-symmetric shallow bimetallic shells with circular opening at the top of the shell. According to the third order theory by the Czech researcher E. Chawalla,... more
    The paper deals with stresses, strains and buckling conditions in the thin axi-symmetric shallow bimetallic shells with circular opening at the top of the shell. According to the third order theory by the Czech researcher E. Chawalla, which takes into account the equilibrium state of forces and moments acting on the deformed system, the paper presents a model for mathematical
    Purpose: Phenomena of deformation and fracture of two-phase metal matrix materials are two very interesting problems in the sceintific field of materials science and engineering. The study of these two issues can greatly contribute to... more
    Purpose: Phenomena of deformation and fracture of two-phase metal matrix materials are two very interesting problems in the sceintific field of materials science and engineering. The study of these two issues can greatly contribute to better mechanical and technological properties of two-phase metal matrix materials. Design/methodology/approach: This work presents macroscopic models of two-phase metal matrix material, composed of ductile matrix and more rigid and hard inclusions (inserts) of secondary phase, prepared for the tensile deformation. These types of models are enlarged for two to three orders of magnitude comparing to the real copper matrix materials, and they are suitable for numerical as well as experimental modelling and simulation. Findings: The basic aim of the numerical and experimental modelling is in the observation of the matrix material flow, and in analysis of the stress-strain state in the matrix. Research limitations/implications: Deficiencies in FEA of the t...
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    This article investigates a method for obtaining all equilibrium configurations of a cantilever beam subjected to an end load with a constant angle of inclination. The formulation is based on plane finite-strain beam theory in the elastic... more
    This article investigates a method for obtaining all equilibrium configurations of a cantilever beam subjected to an end load with a constant angle of inclination. The formulation is based on plane finite-strain beam theory in the elastic domain. An example of a cantilever beam subjected to a horizontal pressure force is discussed in detail.
    In this article uniaxial constrained recovery is modelled using the theory of generalized plasticity, which was developed by J. Lubliner and F. Auricchio. As a mechanical obstacle that delays free recovery in a shape memory alloy wire, a... more
    In this article uniaxial constrained recovery is modelled using the theory of generalized plasticity, which was developed by J. Lubliner and F. Auricchio. As a mechanical obstacle that delays free recovery in a shape memory alloy wire, a bias spring made of an ordinary material is used. Two flow rules are used in the modelling: linear and exponential.
    ABSTRACT In this contribution, we discuss the stress, deformation, and snap-through conditions of thin, axi-symmetric, shallow bimetallic shells of so-called parabolic-conic and plate-parabolic type shells loaded by thermal loading.... more
    ABSTRACT In this contribution, we discuss the stress, deformation, and snap-through conditions of thin, axi-symmetric, shallow bimetallic shells of so-called parabolic-conic and plate-parabolic type shells loaded by thermal loading. According to the theory of the third order that takes into account the balance of forces on a deformed body, we present a model with a mathematical description of the system geometry, displacements, stress, and thermoelastic deformations. The equations are based on the large displacements theory. We numerically calculate the deformation curve and the snap-through temperature using the fourth-order Runge-Kutta method and a nonlinear shooting method. We show how the temperature of both snap-through depends on the point where one type of the rotational curve transforms into another.
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    ABSTRACT The dynamic aeroelastic behavior of an elastically supported airfoil is studied in order to investigate the possibilities of increasing critical flutter speed by exploiting its chord-wise flexibility. The flexible airfoil concept... more
    ABSTRACT The dynamic aeroelastic behavior of an elastically supported airfoil is studied in order to investigate the possibilities of increasing critical flutter speed by exploiting its chord-wise flexibility. The flexible airfoil concept is implemented using a rigid airfoil-shaped leading edge, and a flexible thin laminated composite plate conformally attached to its trailing edge. The flutter behavior is studied in terms of the number of laminate plies used in the composite plate for a given aeroelastic system configuration. The flutter behavior is predicted by using an eigenfunction expansion approach which is also used to design a laminated plate in order to attain superior flutter characteristics. Such an airfoil is characterized by two types of flutter responses, the classical airfoil flutter and the plate flutter. Analysis shows that a significant increase in the critical flutter speed can be achieved with high plunge and low pitch stiffness in the region where the aeroelastic system exhibits a bimodal flutter behavior, e.g., where the airfoil flutter and the plate flutter occur simultaneously. The predicted flutter behavior of a flexible airfoil is experimentally verified by conducting a series of systematic aeroelastic system configurations wind tunnel flutter campaigns. The experimental investigations provide, for each type of flutter, a measured flutter response, including the one with indicated bimodal behavior.
    ... Images Images, Journal/Book title, Volume, Issue, Page, Search tips. ... NOTATION EH' PP,,P2, P3, P,,P5 x, y, zv tro 01, 02 Modulus of elasticity Tangent modulus Hardening parameter Internal pressure Limit loads as defined ...... more
    ... Images Images, Journal/Book title, Volume, Issue, Page, Search tips. ... NOTATION EH' PP,,P2, P3, P,,P5 x, y, zv tro 01, 02 Modulus of elasticity Tangent modulus Hardening parameter Internal pressure Limit loads as defined ... Plastic yielding was defined by the von Mises yield criterion ...
    ABSTRACT This paper investigates the application of the high-pressure jet assistance (HPJA) in rough turning of Inconel 718 with coated carbide tools. The region of operability, which sets the boundaries of the process parameters, has... more
    ABSTRACT This paper investigates the application of the high-pressure jet assistance (HPJA) in rough turning of Inconel 718 with coated carbide tools. The region of operability, which sets the boundaries of the process parameters, has been experimentally determined using the tool–material pair (TMP) methodology. The assessment of HPJA machining performance is based on response surface methodology (RSM), which integrates a design of experiment (DOE) and a regression modelling technique for fitting a model to experimental. This leads to a new insight into the influence of the cutting process on chip breakability, cutting forces, contact length, surface finish and tool temperature, which are the key machining performance measures.
    ABSTRACT A comprehensive experimental approach to the problem of determining static stability boundary (divergence) or dynamic stability boundary (flutter) of a given multiparameter aeroelastic system in a low speed wind tunnel is... more
    ABSTRACT A comprehensive experimental approach to the problem of determining static stability boundary (divergence) or dynamic stability boundary (flutter) of a given multiparameter aeroelastic system in a low speed wind tunnel is presented. The experimental setup with the corresponding measurement algorithm is based on the well-known theoretical model of an elastically supported typical wing section with two degrees of freedom. The design of the experimental system makes it possible to vary structural parameters within the determined parameter space. An automated measurement algorithm for determination of static or dynamic stability boundary by monitoring the aeroelastic system response to an initial impulse in the time domain is developed. The multiparameter experimental results of the case study using a NACA 0012 airfoil are compared to the analytical solutions of the theoretical model. The comparison shows that the experimental setup represents a reliable platform for aeroelastic wind tunnel test purposes. In addition, series of experiments were conducted to investigate the effect of airfoil thickness distribution on dynamic and static stability boundary. The results are compared to those of the NACA 0012 airfoil.
    In this paper, the principle of relative motion is used to investigate the dynamic response of a spring-frame-supported cantilever simple beam with concentrated mass. Both free vibration and forced vibration caused by the base movement... more
    In this paper, the principle of relative motion is used to investigate the dynamic response of a spring-frame-supported cantilever simple beam with concentrated mass. Both free vibration and forced vibration caused by the base movement are studied. The cantilever simple beam is discretized into a simple beam and a cantilever beam. Therefore, the general analytical solution of homogeneous beams with
    The paper deals with the elastic stability problem of thin annular plates made of moderately orthotropic material. Examples of this kind can be plates with periodically cut, parallel grooves, the areas in-between acting as very low ribs.... more
    The paper deals with the elastic stability problem of thin annular plates made of moderately orthotropic material. Examples of this kind can be plates with periodically cut, parallel grooves, the areas in-between acting as very low ribs. The numerical solutions are obtained on the basis of the energy method. The chosen displacement functions can be used to solve the cases of nonaxisymmetric buckling of the ring in a circular direction for an axisymmetric radial compressive load acting along the edges. The ultimate buckling forces are calculated for the following combinations of boundary conditions: both ring edges are rigidly fixed, the outer edge is rigidly fixed and the inner simply supported and both edges are simply supported. The results analysis has shown that the load carrying capacity depends on the grade of orthotropy which effects a change in the rigidity of the ring.
    ... strain related to the formation of each variant plays a major role in the modelling of the ... These orientations are randomly chosen to induce no particular texture in the material. ... of the phase transformation kinematic 250 0 50... more
    ... strain related to the formation of each variant plays a major role in the modelling of the ... These orientations are randomly chosen to induce no particular texture in the material. ... of the phase transformation kinematic 250 0 50 100 150 200 Stress (MPa) Figure 5: Evolution of the ...
    ... 002497 NEW ANALYTICAL PROCEDURE TO DETERMINE STRESSSTRAIN CURVE FROM SPHERICAL INDENTATION DATA B. TALJAT, T. ZACHARIA Oak Ridge ... Several other authors (Francis, 1976; Johnson, 1970; Sinclair et al., 1985; Au et al., 1980) have... more
    ... 002497 NEW ANALYTICAL PROCEDURE TO DETERMINE STRESSSTRAIN CURVE FROM SPHERICAL INDENTATION DATA B. TALJAT, T. ZACHARIA Oak Ridge ... Several other authors (Francis, 1976; Johnson, 1970; Sinclair et al., 1985; Au et al., 1980) have also worked on ...