BULGARIAN ACADEMY OF SCIENCES NATIONAL COMMITTEE OF THEORETICAL AND APPLIED MECHANICS Journal of Theoretical and Applied Mechanics
Print ISSN: 0861-6663 Online ISSN: 1314-8710
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JTAM, Sofia, vol. 52 Issue 4 (2022) |
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PROF. DSC YACHKO IVANOV, MEMBER OF THE BULGARIAN ACADEMY OF SCIENCES, AND HIS REMARKABLE SCIENTIFIC CAREER Ana Yanakieva, Robert Kazandjiev Institute of Mechanics, Bulgarian Academy of Sciences, Acad. G. Bonchev St., Bl. 4, 1113 Sofia, Bulgaria
Academician Yachko Ivanov turned 90 in September
2022. We are pleased to present a short interview with the jubilee outlining
the basic achievements of his remarkable scientific carrier.
JTAM, Sofia, vol. 52 Issue 4 pp. 297-304 (2022), [Full Article]
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FREQUENCIES OF TRIANGULAR PLATE WITH TWO-DIMENSIONAL PARABOLIC THICKNESS UNDER TEMPERATURE FIELD Nisha Dagar1, Reeta Bhardwaj1, Naveen Mani2, Kamal Kumar1, Sudeshna Ghosh1, Amit Sharma1, Lokesh Singh3 1Department of Mathematics, Amity University Haryana, Gurugram, India 2Department of Mathematics, Chandigarh University, Chandigarh, India 3Faculty of Engineering and Technology, Villa College, Maldives
The effect of two-dimensional parabolic thickness on frequencies
of triangular plate (isosceles, right angled, and scalene triangle) is
investigated for clamped edge condition under one dimensional temperature
field. First three modes of vibration are computed on different variation of
plate parameters using Rayleigh-Ritz method. The objective of this study is
to illustrate a numerical data in the form of mode frequencies and showing
how variation in mode frequencies can be control by choosing an appropriate
variation in plate parameters. A comparative study of the frequencies with
other available results is also shown here.
JTAM, Sofia, vol. 52 Issue 4 pp. 305-316 (2022), [Full Article]
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HIGH LIFT CONTROL WITH A CFJ AROUND A NACA 4415 AIRFOIL Zakaria Imine, Mahi Senouci, Sidi Mohamed Amine Meftah Aeronautics and Propulsive Systems Laboratory. Faculté de Génie Mécanique Université des Sciences et de la Technologie D'Oran Mohamed BOUDIAF BP1505 El M'nouar Oran-31000, Algeria
An active concept of lift control around a NACA 4415
airfoil has been presented in this paper. On the upper surface, geometric
modifications were implemented where the blowing and suction were localized
relative to the leading edge. In order to validate the mathematical model, a
baseline NACA 4415 airfoil was examined and compared with experimental data.
Several numerical investigations were considered in which the blowing's
localization and momentum coefficient were modified. These configurations
were tested at a velocity of 21 meters per second with angles of attack
ranging from 0 to 40 degrees. The CFD results show that the CFJ concept is
quite promising, and that by pushing the stall to atypical angles of attack,
it can offer a significant increase in lift force and a delay in boundary
layer separation. However, several analytical correlations for predicting
the coefficient of maximum lift as a function of the blowing position and
the coefficient of momentum have been established.
JTAM, Sofia, vol. 52 Issue 4 pp. 317-334 (2022), [Full Article]
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DYNAMIC NANO-CRACKS INTERACTION IN GRADED MAGNETOELECTROELASTIC SOLID Tsviatko V. Rangelov, Yonko D. Stoynov, Petia S. Dineva 1Institute of Mathematics and Informatics, Bulgarian Academy of Sciences, Sofia 1113, Bulgaria 2Faculty of Applied Mathematics and Informatics, Technical University, Sofia 1000, Bulgaria 3Institute of Mechanics, Bulgarian Academy of Sciences, Sofia 1113, Bulgaria
Dynamic fracture behaviour of multiple anti-plane nano-cracks in infinite functionally graded magnetoelectroelastic (MEE) solid under excitation of time-harmonic SH-wave is studied. The applied approach is based on the non-hypersingular traction based boundary integral equation method (BIEM) for the graded bulk MEE solid extended with the non-classical boundary conditions and the localized constitutive law for the MEE matrix-nanocrack interface within the framework of the Gurtin-Murdoch theory. The formulation allows for an exponential variation of the material properties in an arbitrary direction. The boundary integral equation (BIE) system is treated by using the frequency dependent fundamental solution derived analytically by Fourier transforms. The numerical solution provides displacements and tractions at any point in the infinite graded solid as well as the generalized crack opening displacements from which the generalized stress concentrations are determined. Simulations for different nano-cracks configurations such as collinear, parallel or nanocracks in arbitrary position to each other are presented and discussed. They demonstrate among others the MEE coupling, the frequency dependent shielding and amplification effects resulting from nano-cracks interaction and reveal the sensitivity of the stress concentration factors to the complex influence of wave-crack and crack-crack interactions, existence of material gradient and surface elasticity effects.
JTAM, Sofia, vol. 52 Issue 4 pp. 335-350 (2022), [Full Article]
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SAFETY ZONE WITHIN THE LOAD SPACE OF DIFFUSIVELY SURFACE-REINFORCED STRUCTURAL COMPONENTS Ana Yanakieva, Anguel Baltov, Gergana Nikolova Institute of Mechanics, Bulgarian Academy of Sciences, Acad. G. Bontchev St., bl. 4, 1113 Sofia, Bulgaria
The paper proposes a new Methodology for determining the
safety zone of a structural element in the load space. To calculate the
load-bearing capacity of the selected composite structural element, the
Approximate Computational Model (ACM) created by the authors is applied,
adapted, and extended for strength load-bearing capacity. The structural
element is reinforced on both sides with a reinforcing substance and
subjected to overloads (loads above the permissible norms). Through
appropriately selected dimensionless parameters, a load space is built, and
boundary surfaces of load-bearing capacity are built in it. These surfaces
enclose the required volume safety zone.
JTAM, Sofia, vol. 52 Issue 4 pp. 351-364 (2022), [Full Article]
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INFLUENCE OF TYPE OF ADHESIVE ON THE INTERFACE DEBONDING OF A BaTiO3/EPOXY STRUCTURE UNDER TIME HARMONIC MECHANICAL LOAD AND ELECTRIC FIELD AT ENVIRONMENTAL CONDITIONS Tatyana Petrova1, Elisaveta Kirilova1, Wilfried Becker2, Jordanka Ivanova3 1Bulgarian Academy of Sciences, Institute of Chemical Engineering, Acad. G. Bonchev Str., bl. 103, 1113 Sofia, Bulgaria 2Technical University of Darmstadt, Franziska-Braun-Straße 7, 64287 Darmstadt, Germany 3European Polytechnical University, 23 Sv. Sv. Kiril i Metodiy Str., 2300 Pernik, Bulgaria
The study deals with investigation of the effect
of the used adhesive upon the interface delamination at adhesively bonded
piezoelectric patch/layer structure BaTiO3/Epoxy subjected to
time harmonic mechanical load and electric field at environmental
conditions. This is needed for a prediction of conditions, at which these
type of structures work safely (without failure). For the interface shear
stress in the overlap zone of structure, at two different thicknesses of its
adherends and three adhesives used, a solution method based on shear lag and
Fourier method has been applied. The types of solutions obtained depend
mainly on the adherends' thickness, the magnitude and frequency of the
applied mechanical loading and the shear modulus of the used adhesive. Based
on the analysis conducted it has been shown that with increasing magnitude
and frequency of applied mechanical load, the delamination length also
increased. The delamination could be avoided if the stronger adhesives and
thicker adherends are chosen. The debond length is highly dependent on the
magnitude of electric displacement. The analytical equation for resonant
frequencies in the considered structure is developed on the base of obtained
solutions and they are calculated at all three investigated adhesives.
JTAM, Sofia, vol. 52 Issue 4 pp. 365-380 (2022), [Full Article]
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INVESTIGATION OF GLASSY CARBON COATING DEPOSITED ON TITANIUM ALLOY: MICROSTRUCTURE AND MECHANICAL PROPERTIES Vladimir Petkov1, Mihaela Aleksandrova1, Veselin Petkov1, Dimitar Teodosiev2, Anna Bouzekova-Penkova2 1Bulgarian Academy of Sciences, Institute of Metal Science,\\ Equipment and Technology with Hydroaerodynamic Center, "Acad. Angel Balevski'', 67 "Shipchenski Prohod'' Blvd, 1574 Sofia, Bulgaria 2Bulgarian Academy of Sciences, Space Research and Technology Institute, 1. "Acad. Georgy Bonchev'', 1113 Sofia, Bulgaria
The deposition of glassy carbon coating on the
widely applied in implantology titanium alloy – Ti 6V 4Al, is performed by a
novel original thermo-chemical method, developed in the Bulgarian Academy of
Sciences. The deposition of glassy carbon was carried out in a protective
inert environment of argon at high temperature around 1000°C. The
combination of biocompatible carbon containing coating and biocompatible
titanium alloy represents an innovative implant material for medical use. An
important aspect of the new material development process is the study of the
mechanical properties and microstructure. Therefore, the microstructure and
the mechanical characteristics of the obtained composite biocompatible
material, consisting of titanium matrix and glassy carbon coating, were
studied in the present work. The microstructure of the coating and its
elemental composition were examined by metallographic microscope and by
SEM-EDS analysis. Mechanical tests have also been performed in order to
determine and compare the ultimate tensile strength and tensile yield
strength of titanium alloy samples with and without glassy carbon cover. The
hardness and the modulus of elasticity of the considered materials are
determined by instrumented indentation technique.
JTAM, Sofia, vol. 52 Issue 4 pp. 381-392 (2022), [Full Article]
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