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The dynamics of coupled elements’ ensembles are investigated in the context of description of spatio-temporal processes in the myocardium. Basic element is map-based model constructed by simplification and reduction of Luo-Rudy model. In particular, capabilities of the model in replication of different regimes of cardiac activity are shown, including excitable and oscillatory regimes. The dynamics of 1D and 2D lattices of coupled oscillatory elements with a random distribution of individual frequencies are considered. Effects of cluster synchronization and transition to global synchronization by increasing of coupling strength are discussed. Impulse propagation in the chain of excitable cells has been observed. Analysis of 2D lattice of excitable elements with target and spiral waves have been made. The characteristics of the spiral wave has been analyzed in depending on the individual parameters of the map and coupling strength between elements of the lattice. A study of mixed ensembles consisting of excitable and oscillatory elements with a gradient changing of the properties have been made, including the task for description of normal and pathological activity of the sinoatrial node.

The temporal variability of exergy of short-wave and long-wave radiation and its relationships with sensible heat, water vapor (H₂O) and carbon dioxide (CO₂) fluxes on a recently clear-cut area in a mixed coniferous and small-leaved forest in the Tver region is discussed. On the basis of the analysis of radiation and exergy efficiency coefficients suggested by Yu.M. Svirezhev it was shown that during the first eight months after clearcutting the forest ecosystem functions as a "heat engine" i.e. the processes of energy dissipation dominated over processes of biomass production. To validate the findings the statistical analysis of temporary variability of meteorological parameters, as well as, daily fluxes of sensible heat, H₂O and CO₂ was provided using the trigonometrical polynomials. The statistical models that are linearly depended on an exergy of short-wave and long-wave radiation were obtained for mean daily values of CO₂ fluxes, gross primary production of regenerated vegetation and sensible heat fluxes. The analysis of these dependences is also confirmed the results obtained from processing the radiation and exergy efficiency coefficients. The splitting the time series into separate time intervals, e.g. “spring–summer” and “summer–autumn”, allowed revealing that the statistically significant relationships between atmospheric fluxes and exergy were amplified in summer months as the clear-cut area was overgrown by grassy and young woody vegetation. The analysis of linear relationships between time-series of latent heat fluxes and exergy showed their statistical insignificance. The linear relationships between latent heat fluxes and temperature were in turn statistically significant. The air temperature was a key factor improving the accuracy of the models, whereas effect of exergy was insignificant. The results indicated that at the time of active vegetation regeneration within the clear-cut area the seasonal variability of surface evaporation is mainly governed by temperature variation.

In the last few years, significant progress has been observed in the field of rotating detonation engines for aircrafts. Scientific laboratories around the world conduct both fundamental researches related, for example, to the issues of effective mixing of fuel and oxidizer with the separate supply, and applied development of existing prototypes. The paper provides a brief overview of the main results of the most significant recent computational work on the study of propagation of a onedimensional pulsating gaseous detonation wave in a non-uniform medium. The general trends observed by the authors of these works are noted. In these works, it is shown that the presence of parameter perturbations in front of the wave front can lead to regularization and to resonant amplification of pulsations behind the detonation wave front. Thus, there is an appealing opportunity from a practical point of view to influence the stability of the detonation wave and control it. The aim of the present work is to create an instrument to study the gas-dynamic mechanisms of these effects.

The mathematical model is based on one-dimensional Euler equations supplemented by a one-stage model of the kinetics of chemical reactions. The defining system of equations is written in the shock-attached frame that leads to the need to add a shock-change equations. A method for integrating this equation is proposed, taking into account the change in the density of the medium in front of the wave front. So, the numerical algorithm for the simulation of detonation wave propagation in a non-uniform medium is proposed.

Using the developed algorithm, a numerical study of the propagation of stable detonation in a medium with variable density as carried out. A mode with a relatively small oscillation amplitude is investigated, in which the fluctuations of the parameters behind the detonation wave front occur with the frequency of fluctuations in the density of the medium. It is shown the relationship of the oscillation period with the passage time of the characteristics C₊ and C₀ over the region, which can be conditionally considered an induction zone. The phase shift between the oscillations of the velocity of the detonation wave and the density of the gas before the wave is estimated as the maximum time of passage of the characteristic C₊ through the induction zone.

The paper is a study of the mathematical model and kinematics of a parallel spherical manipulator. This type of manipulator was proposed back in the 80s of the last century and has since found application in exoskeletons and rehabilitation robots due to its structure, which allows imitating natural joint movements of the human body.

The Parallel Spherical Manipulator is a robot with three legs and two platforms, a base platform and a mobile platform. Its legs consist of two support links that are arc-shaped. Mathematically, the manipulator can be described using two virtual pyramids that are placed on top of each other.

The paper considers two types of manipulator configurations: classical and asymmetric, and solves basic kinematic problems for each. The study shows that the asymmetric design of the manipulator has the maximum workspace, especially when the motors are mounted at the joints of the manipulator’s links inside legs.

To optimize the parameters of the parallel spherical manipulator, we introduced a metric of usable workspace volume. This metric represents the volume of the sector of the sphere in which the robot does not experience internal collisions or singular states. There are three types of singular states possible within a parallel spherical manipulator — serial, parallel, and mixed singularity. We used all three types of singularities to calculate the useful volume. In our research work, we solved the problem related to maximizing the usable volume of the workspace.

Through our research work, we found that the asymmetric configuration of the spherical manipulator maximizes the workspace when the motors are located at the articulation point of the robot leg support arms. At the same time, the parameter $\beta_1$ must be zero degrees to maximize the workspace. This allowed us to create a prototype robot in which we eliminated the use of lower links in legs in favor of a radiused rail along which the motors run. This allowed us to reduce the linear dimensions of the robot itself and gain on the stiffness of the structure.

The results obtained can be used to optimize the parameters of the parallel spherical manipulator in various industrial and scientific applications, as well as for further research of other types of parallel robots and manipulators.

Numerical investigation of mixing non-isothermal streams of sodium coolant in a T-branch is carried out in the FlowVision CFD software. This study is aimed at argumentation of applicability of different approaches to prediction of oscillating behavior of the flow in the mixing zone and simulation of temperature pulsations. The following approaches are considered: URANS (Unsteady Reynolds Averaged Navier Stokers), LES (Large Eddy Simulation) and quasi-DNS (Direct Numerical Simulation). One of the main tasks of the work is detection of the advantages and drawbacks of the aforementioned approaches.

Numerical investigation of temperature pulsations, arising in the liquid and T-branch walls from the mixing of non-isothermal streams of sodium coolant was carried out within a mathematical model assuming that the flow is turbulent, the fluid density does not depend on pressure, and that heat exchange proceeds between the coolant and T-branch walls. Model LMS designed for modeling turbulent heat transfer was used in the calculations within URANS approach. The model allows calculation of the Prandtl number distribution over the computational domain.

Preliminary study was dedicated to estimation of the influence of computational grid on the development of oscillating flow and character of temperature pulsation within the aforementioned approaches. The study resulted in formulation of criteria for grid generation for each approach.

Then, calculations of three flow regimes have been carried out. The regimes differ by the ratios of the sodium mass flow rates and temperatures at the T-branch inlets. Each regime was calculated with use of the URANS, LES and quasi-DNS approaches.

At the final stage of the work analytical comparison of numerical and experimental data was performed. Advantages and drawbacks of each approach to simulation of mixing non-isothermal streams of sodium coolant in the T-branch are revealed and formulated.

It is shown that the URANS approach predicts the mean temperature distribution with a reasonable accuracy. It requires essentially less computational and time resources compared to the LES and DNS approaches. The drawback of this approach is that it does not reproduce pulsations of velocity, pressure and temperature.

The LES and DNS approaches also predict the mean temperature with a reasonable accuracy. They provide oscillating solutions. The obtained amplitudes of the temperature pulsations exceed the experimental ones. The spectral power densities in the check points inside the sodium flow agree well with the experimental data. However, the expenses of the computational and time resources essentially exceed those for the URANS approach in the performed numerical experiments: 350 times for LES and 1500 times for ·DNS.

The paper presents a physical and numerical analysis of the dynamics and radiation of explosion products formed during the Russian-American experiment in the ionosphere using an explosive generator based on hexogen (RDX) and trinitrotoluene (TNT). The main attention is paid to the radiation of the perturbed region and the dynamics of the products of explosion (PE). The detailed chemical composition of the explosion products is analyzed and the initial concentrations of the most important molecules capable of emitting in the infrared range of the spectrum are determined, and their radiative constants are given. The initial temperature of the explosion products and the adiabatic exponent are determined. The nature of the interpenetration of atoms and molecules of a highly rarefied ionosphere into a spherically expanding cloud of products is analyzed. An approximate mathematical model of the dynamics of explosion products under conditions of mixing rarefied ionospheric air with them has been developed and the main thermodynamic characteristics of the system have been calculated. It is shown that for a time of 0,3–3 sec there is a significant increase in the temperature of the scattering mixture as a result of its deceleration. In the problem under consideration the explosion products and the background gas are separated by a contact boundary. To solve this two-region gas dynamic problem a numerical algorithm based on the Lagrangian approach was developed. It was necessary to fulfill special conditions at the contact boundary during its movement in a stationary gas. In this case there are certain difficulties in describing the parameters of the explosion products near the contact boundary which is associated with a large difference in the size of the mass cells of the explosion products and the background due to a density difference of 13 orders of magnitude. To reduce the calculation time of this problem an irregular calculation grid was used in the area of explosion products. Calculations were performed with different adiabatic exponents. The most important result is temperature. It is in good agreement with the results obtained by the method that approximately takes into account interpenetration. The time behavior of the IR emission coefficients of active molecules in a wide range of the spectrum is obtained. This behavior is qualitatively consistent with experiments for the IR glow of flying explosion products.

State-of-the-art localization and mapping approaches for augmented (AR) and mixed (MR) reality devices are based on the extraction of local features from the camera. Along with this, modern AR/MR devices allow you to build a three-dimensional mesh of the surrounding space. However, the existing methods do not solve the problem of global device co-localization due to the use of different methods for extracting computer vision features. Using a space map from a 3D mesh, we can solve the problem of collaborative global localization of AR/MR devices. This approach is independent of the type of feature descriptors and localisation and mapping algorithms used onboard the AR/MR device. The mesh can be reduced to a point cloud, which consists of only the vertices of the mesh. We propose an approach for collaborative localization of AR/MR devices using point clouds that are independent of algorithms onboard the device. We have analyzed various point cloud registration algorithms and discussed their limitations for the problem of global co-localization of AR/MR devices indoors.

We consider “predator – prey” model taking into account the competition of prey, predator for different from the prey resources, and their interaction described by the second type Holling trophic function. An analysis of the attractors is carried out depending on the coefficient of competition of predators. In the deterministic case, this model demonstrates the complex behavior associated with the local (Andronov –Hopf and saddlenode) and global (birth of a cycle from a separatrix loop) bifurcations. An important feature of this model is the disappearance of a stable cycle due to a saddle-node bifurcation. As a result of the presence of competition in both populations, parametric zones of mono- and bistability are observed. In parametric zones of bistability the system has either coexisting two equilibria or a cycle and equilibrium. Here, we investigate the geometrical arrangement of attractors and separatrices, which is the boundary of basins of attraction. Such a study is an important component in understanding of stochastic phenomena. In this model, the combination of the nonlinearity and random perturbations leads to the appearance of new phenomena with no analogues in the deterministic case, such as noise-induced transitions through the separatrix, stochastic excitability, and generation of mixed-mode oscillations. For the parametric study of these phenomena, we use the stochastic sensitivity function technique and the confidence domain method. In the bistability zones, we study the deformations of the equilibrium or oscillation regimes under stochastic perturbation. The geometric criterion for the occurrence of such qualitative changes is the intersection of confidence domains and the separatrix of the deterministic model. In the zone of monostability, we evolve the phenomena of explosive change in the size of population as well as extinction of one or both populations with minor changes in external conditions. With the help of the confidence domains method, we solve the problem of estimating the proximity of a stochastic population to dangerous boundaries, upon reaching which the coexistence of populations is destroyed and their extinction is observed.

In this article we consider min-min type of problems or minimization by two groups of variables. In some way it is similar to classic min-max saddle point problem. Although, saddle point problems are usually more difficult in some way. Min-min problems may occur in case if some groups of variables in convex optimization have different dimensions or if these groups have different domains. Such problem structure gives us an ability to split the main task to subproblems, and allows to tackle it with mixed oracles. However existing articles on this topic cover only zeroth and first order oracles, in our work we consider high-order tensor methods to solve inner problem and fast gradient method to solve outer problem.

We assume, that outer problem is constrained to some convex compact set, and for the inner problem we consider both unconstrained case and being constrained to some convex compact set. By definition, tensor methods use high-order derivatives, so the time per single iteration of the method depends a lot on the dimensionality of the problem it solves. Therefore, we suggest, that the dimension of the inner problem variable is not greater than 1000. Additionally, we need some specific assumptions to be able to use mixed oracles. Firstly, we assume, that the objective is convex in both groups of variables and its gradient by both variables is Lipschitz continuous. Secondly, we assume the inner problem is strongly convex and its gradient is Lipschitz continuous. Also, since we are going to use tensor methods for inner problem, we need it to be p-th order Lipschitz continuous ($p > 1$). Finally, we assume strong convexity of the outer problem to be able to use fast gradient method for strongly convex functions.

We need to emphasize, that we use superfast tensor method to tackle inner subproblem in unconstrained case. And when we solve inner problem on compact set, we use accelerated high-order composite proximal method.

Additionally, in the end of the article we compare the theoretical complexity of obtained methods with regular gradient method, which solves the mentioned problem as regular convex optimization problem and doesn’t take into account its structure (Remarks 1 and 2).

The paper gives a detailed description of the developed methods for simulating the turbulent flow around a helicopter rotor and calculating its aerodynamic characteristics. The system of Reynolds-averaged Navier – Stokes equations for a viscous compressible gas closed by the Spalart –Allmaras turbulence model is used as the basic mathematical model. The model is formulated in a non-inertial rotating coordinate system associated with a rotor. To set the boundary conditions on the surface of the rotor, wall functions are used.

The numerical solution of the resulting system of differential equations is carried out on mixed-element unstructured grids including prismatic layers near the surface of a streamlined body.The numerical method is based on the original vertex-centered finite-volume EBR schemes. A feature of these schemes is their higher accuracy which is achieved through the use of edge-based reconstruction of variables on extended quasi-onedimensional stencils, and a moderate computational cost which allows for serial computations. The methods of Roe and Lax – Friedrichs are used as approximate Riemann solvers. The Roe method is corrected in the case of low Mach flows. When dealing with discontinuities or solutions with large gradients, a quasi-one-dimensional WENO scheme or local switching to a quasi-one-dimensional TVD-type reconstruction is used. The time integration is carried out according to the implicit three-layer second-order scheme with Newton linearization of the system of difference equations. To solve the system of linear equations, the stabilized conjugate gradient method is used.

The numerical methods are implemented as a part of the in-house code NOISEtte according to the two-level MPI–OpenMP parallel model, which allows high-performance computations on meshes consisting of hundreds of millions of nodes, while involving hundreds of thousands of CPU cores of modern supercomputers.

Based on the results of numerical simulation, the aerodynamic characteristics of the helicopter rotor are calculated, namely, trust, torque and their dimensionless coefficients.

Validation of the developed technique is carried out by simulating the turbulent flow around the Caradonna – Tung two-blade rotor and the KNRTU-KAI four-blade model rotor in hover mode mode, tail rotor in duct, and rigid main rotor in oblique flow. The numerical results are compared with the available experimental data.