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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.

A promising method of increasing precipitation in arid climates is the method of creating a vertical high-temperature jet seeded by hygroscopic aerosol. Such an installation makes it possible to create artificial clouds with the possibility of precipitation formation in a cloudless atmosphere, unlike traditional methods of artificial precipitation enhancement, which provide for increasing the efficiency of precipitation formation only in natural clouds by seeding them with nuclei of crystallization and condensation. To increase the power of the jet, calcium chloride, carbamide, salt in the form of a coarse aerosol, as well as NaCl/TiO₂ core/shell novel nanopowder, which is capable of condensing much more water vapor than the listed types of aerosols, are added. Dispersed inclusions in the jet are also centers of crystallization and condensation in the created cloud to increase the possibility of precipitation. To simulate convective flows in the atmosphere, a mathematical model of FlowVision large-scale atmospheric flows is used, the solution of the equations of motion, energy and mass transfer is carried out in relative variables. The statement of the problem is divided into two parts: the initial jet model and the FlowVision large-scale atmospheric model. The lower region, where the initial high-speed jet flows, is calculated using a compressible formulation with the solution of the energy equation with respect to the total enthalpy. This division of the problem into two separate subdomains is necessary in order to correctly carry out the numerical calculation of the initial turbulent jet at high velocity (M > 0.3). The main mathematical dependencies of the model are given. Numerical experiments were carried out using the presented model, experimental data from field tests of the installation for creating artificial clouds were taken for the initial data. A good agreement with the experiment is obtained: in 55% of the calculations carried out, the value of the vertical velocity at a height of 400 m (more than 2 m/s) and the height of the jet rise (more than 600 m) is within an deviation of 30% of the experimental characteristics, and in 30% of the calculations it is completely consistent with the experiment. The results of numerical simulation allow evaluating the possibility of using the high-speed jet method to stimulate artificial updrafts and to create precipitation. The calculations were carried out using FlowVision CFD software on SUSU Tornado supercomputer.

The results of determination of the risk of cardiovascular failure of young athletes and adolescents in stressful physical activity have been demonstrated. The method of screening diagnostics of the risk of developing heart failure has been described. The results of contactless measurement of the form of the pulse wave of the radial artery using semiconductor laser autodyne have been presented. In the measurements used laser diode type RLD-650 specifications: output power of 5 mW, emission wavelength 654 nm. The problem was solved by the reduced form of the reflector movement, which acts as the surface of the skin of the human artery, tested method of assessing the risk of cardiovascular disease during exercise and the analysis of the results of its application to assess the risk of cardiovascular failure reactions of young athletes. As analyzed parameters were selected the following indicators: the steepness of the rise in the systolic portion of the fast and slow phase, the rate of change in the pulse wave catacrota variability of cardio intervals as determined by the time intervals between the peaks of the pulse wave. It analyzed pulse wave form on its first and second derivative with respect to time. The zeros of the first derivative of the pulse wave allow to set aside time in systolic rise. A minimum of the second derivative corresponds to the end of the phase and the beginning of the slow pressure build-up in the systole. Using the first and second derivative of the pulse wave made it possible to separately analyze the pulse wave form phase of rapid and slow pressure increase phase during systolic expansion. It has been established that the presence of anomalies in the form of the pulse wave in combination with vagotonic nervous regulation of the cardiovascular system of a patient is a sign of danger collapse of circulation during physical exercise.

The work is devoted to the construction and analysis of difference schemes for a system of hemodynamic equations obtained by averaging the hydrodynamic equations of a viscous incompressible fluid over the vessel cross-section. Models of blood as an ideal and as a viscous Newtonian fluid are considered. Difference schemes that approximate equations with second order on the spatial variable are proposed. The computational algorithms of the constructed schemes are based on the method of splitting on physical processes. According to this approach, at one time step, the model equations are considered separately and sequentially. The practical implementation of the proposed schemes at each time step leads to a sequential solution of two linear systems with tridiagonal matrices. It is demonstrated that the schemes are $\rho$-stable under minor restrictions on the time step in the case of sufficiently smooth solutions.

For the problem with a known analytical solution, it is demonstrated that the numerical solution has a second order convergence in a wide range of spatial grid step. The proposed schemes are compared with well-known explicit schemes, such as the Lax – Wendroff, Lax – Friedrichs and McCormack schemes in computational experiments on modeling blood flow in model vascular systems. It is demonstrated that the results obtained using the proposed schemes are close to the results obtained using other computational schemes, including schemes constructed by other approaches to spatial discretization. It is demonstrated that in the case of different spatial grids, the time of computation for the proposed schemes is significantly less than in the case of explicit schemes, despite the need to solve systems of linear equations at each step. The disadvantages of the schemes are the limitation on the time step in the case of discontinuous or strongly changing solutions and the need to use extrapolation of values at the boundary points of the vessels. In this regard, problems on the adaptation of splitting schemes for problems with discontinuous solutions and in cases of special types of conditions at the vessels ends are perspective for further research.

We consider strongly-convex-strongly-concave saddle-point problems with general non-bilinear objective and different condition numbers with respect to the primal and dual variables. First, we consider such problems with smooth composite terms, one of which has finite-sum structure. For this setting we propose a variance reduction algorithm with complexity estimates superior to the existing bounds in the literature. Second, we consider finite-sum saddle-point problems with composite terms and propose several algorithms depending on the properties of the composite terms. When the composite terms are smooth we obtain better complexity bounds than the ones in the literature, including the bounds of a recently proposed nearly-optimal algorithms which do not consider the composite structure of the problem. If the composite terms are prox-friendly, we propose a variance reduction algorithm that, on the one hand, is accelerated compared to existing variance reduction algorithms and, on the other hand, provides in the composite setting similar complexity bounds to the nearly-optimal algorithm which is designed for noncomposite setting. Besides, our algorithms allow one to separate the complexity bounds, i. e. estimate, for each part of the objective separately, the number of oracle calls that is sufficient to achieve a given accuracy. This is important since different parts can have different arithmetic complexity of the oracle, and it is desired to call expensive oracles less often than cheap oracles. The key thing to all these results is our general framework for saddle-point problems, which may be of independent interest. This framework, in turn is based on our proposed Accelerated Meta-Algorithm for composite optimization with probabilistic inexact oracles and probabilistic inexactness in the proximal mapping, which may be of independent interest as well.