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The article is devoted to the construction and investigation of an averaged mathematical model of an aluminum-cobalt-molybdenum hydrocracking catalyst oxidative regeneration. The oxidative regeneration is an effective means of restoring the activity of the catalyst when its granules are coating with coke scurf.

The mathematical model of this process is a nonlinear system of ordinary differential equations, which includes kinetic equations for reagents’ concentrations and equations for changes in the temperature of the catalyst granule and the reaction mixture as a result of isothermal reactions and heat transfer between the gas and the catalyst layer. Due to the heterogeneity of the oxidative regeneration process, some of the equations differ from the standard kinetic ones and are based on empirical data. The article discusses the scheme of chemical interaction in the regeneration process, which the material balance equations are compiled on the basis of. It reflects the direct interaction of coke and oxygen, taking into account the degree of coverage of the coke granule with carbon-hydrogen and carbon-oxygen complexes, the release of carbon monoxide and carbon dioxide during combustion, as well as the release of oxygen and hydrogen inside the catalyst granule. The change of the radius and, consequently, the surface area of coke pellets is taken into account. The adequacy of the developed averaged model is confirmed by an analysis of the dynamics of the concentrations of substances and temperature.

The article presents a numerical experiment for a mathematical model of oxidative regeneration of an aluminum-cobalt-molybdenum hydrocracking catalyst. The experiment was carried out using the Kutta–Merson method. This method belongs to the methods of the Runge–Kutta family, but is designed to solve stiff systems of ordinary differential equations. The results of a computational experiment are visualized.

The paper presents the dynamics of the concentrations of substances involved in the oxidative regeneration process. A conclusion on the adequacy of the constructed mathematical model is drawn on the basis of the correspondence of the obtained results to physicochemical laws. The heating of the catalyst granule and the release of carbon monoxide with a change in the radius of the granule for various degrees of initial coking are analyzed. There are a description of the results.

In conclusion, the main results and examples of problems which can be solved using the developed mathematical model are noted.

Laser damage to transparent solids is a major limiting factor output power of laser systems. For laser rangefinders, the most likely destruction cause of elements of the optical system (lenses, mirrors) actually, as a rule, somewhat dusty, is not an optical breakdown as a result of avalanche, but such a thermal effect on the dust speck deposited on an element of the optical system (EOS), which leads to its ignition. It is the ignition of a speck of dust that initiates the process of EOS damage.

The corresponding model of this process leading to the ignition of a speck of dust takes into account the nonlinear Stefan –Boltzmann law of thermal radiation and the infinite thermal effect of periodic radiation on the EOS and the speck of dust. This model is described by a nonlinear system of differential equations for two functions: the EOS temperature and the dust particle temperature. It is proved that due to the accumulating effect of periodic thermal action, the process of reaching the dust speck ignition temperature occurs almost at any a priori possible changes in this process of the thermophysical parameters of the EOS and the dust speck, as well as the heat exchange coefficients between them and the surrounding air. Averaging these parameters over the variables related to both the volume and the surfaces of the dust speck and the EOS is correct under the natural constraints specified in the paper. The entire really significant spectrum of thermophysical parameters is covered thanks to the use of dimensionless units in the problem (including numerical results).

A thorough mathematical study of the corresponding nonlinear system of differential equations made it possible for the first time for the general case of thermophysical parameters and characteristics of the thermal effect of periodic laser radiation to find a formula for the value of the permissible radiation intensity that does not lead to the destruction of the EOS as a result of the ignition of a speck of dust deposited on the EOS. The theoretical value of the permissible intensity found in the general case in the special case of the data from the Grasse laser ranging station (south of France) almost matches that experimentally observed in the observatory.

In parallel with the solution of the main problem, we derive a formula for the power absorption coefficient of laser radiation by an EOS expressed in terms of four dimensionless parameters: the relative intensity of laser radiation, the relative illumination of the EOS, the relative heat transfer coefficient from the EOS to the surrounding air, and the relative steady-state temperature of the EOS.

Certifying a transport airplane for the flights under icing conditions in Russia was carried out within the framework of the requirements of Annex С to the AP-25 Aviation Rules. In force since 2023 to replace AP-25 the new Russian certification document “Airworthiness Standards” (NLG-25) proposes the introduction of Appendix O. A feature of Appendix O is the need to carry out calculations in conditions of high liquid water content and with large water drops (500 microns or more). With such parameters of the dispersed flow, such physical processes as the disruption and splashing of a water film when large drops enter it become decisive. The flow of a dispersed medium under such conditions is essentially polydisperse. This paper describes the modifications of the IceVision technique implemented on the basis of the FlowVision software package for the ice accretion calculations within the framework of Appendix O.

The main difference between the IceVision method and the known approaches is the use of the Volume of fluid (VOF) technology to the shape of ice changes tracking. The external flow around the aircraft is calculated simultaneously with the growth of ice and its heating. Ice is explicitly incorporated in the computational domain; the heat transfer equation is solved in it. Unlike the Lagrangian approaches, the Euler computational grid is not completely rebuilt in the IceVision technique: only the cells containing the contact surface are changed.

The IceVision 2.0 version accounts for stripping the film, as well as bouncing and splashing of falling drops at the surfaces of the aircraft and ice. The diameter of secondary droplets is calculated using known empirical correlations. The speed of the water film flow over the surface is determined taking into account the action of aerodynamic forces, gravity, hydrostatic pressure gradient and surface tension force. The result of taking into account surface tension is the effect of contraction of the film, which leads to the formation of water flows in the form of rivulets and ice deposits in the form of comb-like growths. An energy balance relation is fulfilled on the ice surface that takes into account the energy of falling drops, heat exchange between ice and air, the heat of crystallization, evaporation, sublimation and condensation. The paper presents the results of solving benchmark and model problems, demonstrating the effectiveness of the IceVision technique and the reliability of the obtained results.

Within the framework of the actual problem of comet-asteroid danger, the physical processes causing the destruction and fragmentation of meteor bodies in the Earth’s atmosphere are numerically investigated. Based on the developed physicalmathematical models that determines the movements of space objects of natural origin in the atmosphere and their interaction with it, the fall of three, one of the largest and by some parameters unusual bolides in the history of meteoritics, are considered: Tunguska, Vitim and Chelyabinsk. Their singularity lies in the absence of any material meteorite remains and craters in the area of the alleged crash site for the first two bodies and the non-detection, as it is assumed, of the main mother body for the third body (due to the too small amount of mass of the fallen fragments compared to the estimated mass). The effect of aerodynamic loads and heat flows on these bodies are studied, which leads to intensive surface mass loss and possible mechanical destruction. The velocities of the studied celestial bodies and the change in their masses are determined from the modernized system of equations of the theory of meteoric physics. An important factor that is taken into account here is the variability of the meteorite mass entrainment parameter under the action of heat fluxes (radiation and convective) along the flight path. The process of fragmentation of meteoroids in this paper is considered within the framework of a progressive crushing model based on the statistical theory of strength, taking into account the influence of the scale factor on the ultimate strength of objects. The phenomena and effects arising at various kinematic and physical parameters of each of these bodies are revealed. In particular, the change in the ballistics of their flight in the denser layers of the atmosphere, consisting in the transition from the fall mode to the ascent mode. At the same time, the following scenarios of the event can be realized: 1) the return of the body back to outer space at its residual velocity greater than the second cosmic one; 2) the transition of the body to the orbit of the Earth satellite at a residual velocity greater than the first cosmic one; 3) at lower values of the residual velocity of the body, its return after some time to the fall mode and falling out at a considerable distance from the intended crash site. It is the implementation of one of these three scenarios of the event that explains, for example, the absence of material traces, including craters, in the case of the Tunguska bolide in the vicinity of the forest collapse. Assumptions about the possibility of such scenarios have been made earlier by other authors, and in this paper their implementation is confirmed by the results of numerical calculations.

A three-dimensional (3D) hydrodynamic model to describe the spatial patterns of wind and turbulence characteristics in the atmospheric surface layer over inhomogeneous vegetation cover is presented. To describe the interaction of air flow with vegetation the theory of contrast structures is used. The numerical experiments provided by a developed model to assess the impact of small clear-cutting on wind and turbulent regime in the atmospheric surface layer showed a significant influence of heterogeneous vegetation on the wind field and the turbulent exchange processes between the land surface and the atmosphere. Obtained results give a reasonable agreement with field experimental data and results of numerical experiments provided using alternative models.

The paper presents results of numerical modeling of stress-strain state of jack-up rigs used for shelf hydrocarbon reservoirs exploitation. The work studied the equilibrium stress state of a jack-up rig standing on seafloor and mechanical behavior of the rig under seismic loading. Surface elastic wave caused by a distant earthquake acts a reason for the loading. Stability of jack-up rig is the main topic of the research, as stability can be lost due to redistribution of stresses and strains in the elements of the rig due to seismic loading. Modeling results revealed that seismic loading can indeed lead to intermittent growth of stresses in particular elements of the rig’s support legs resulting into stability loss. These results were obtained using the finite element-based numerical scheme. The paper contains the proof of modeling results convergence obtained from analysis of one problem — the problem of stresses and strains distributions for the contact problem of a rigid cylinder indenting on elastic half space. The comparison between numerical and analytical solutions proved the used numerical scheme to be correct, as obtained results converged. The paper presents an analysis of the different factors influencing the mechanical behavior of the studied system. These factors include the degree of seismic loading, mechanical properties of seafloor sediments, and depth of support legs penetration. The results obtained from numerical modeling made it possible to formulate preliminary conclusions regarding the need to take site-specific conditions into account whenever planning the use of jack-up rigs, especially, in the regions with seismic activity. The approach presented in the paper can be used to evaluate risks related to offshore hydrocarbon reservoirs exploitation and development, while the reported numerical scheme can be used to solve some contact problems of theory of elasticity with the need to analyze dynamic processes.