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Buckling problems of thin elastic shells have become relevant again because of the discrepancies between the standards in many countries on how to estimate loads causing buckling of shallow shells and the results of the experiments on thinwalled aviation structures made of high-strength alloys. The main contradiction is as follows: the ultimate internal stresses at shell buckling (collapsing) turn out to be lower than the ones predicted by the adopted design theory used in the USA and European standards. The current regulations are based on the static theory of shallow shells that was put forward in the 1930s: within the nonlinear theory of elasticity for thin-walled structures there are stable solutions that significantly differ from the forms of equilibrium typical to small initial loads. The minimum load (the lowest critical load) when there is an alternative form of equilibrium was used as a maximum permissible one. In the 1970s it was recognized that this approach is unacceptable for complex loadings. Such cases were not practically relevant in the past while now they occur with thinner structures used under complex conditions. Therefore, the initial theory on bearing capacity assessments needs to be revised. The recent mathematical results that proved asymptotic proximity of the estimates based on two analyses (the three-dimensional dynamic theory of elasticity and the dynamic theory of shallow convex shells) could be used as a theory basis. This paper starts with the setting of the dynamic theory of shallow shells that comes down to one resolving integrodifferential equation (once the special Green function is constructed). It is shown that the obtained nonlinear equation allows for separation of variables and has numerous time-period solutions that meet the Duffing equation with “a soft spring”. This equation has been thoroughly studied; its numerical analysis enables finding an amplitude and an oscillation period depending on the properties of the Green function. If the shell is oscillated with the trial time-harmonic load, the movement of the surface points could be measured at the maximum amplitude. The study proposes an experimental set-up where resonance oscillations are generated with the trial load normal to the surface. The experimental measurements of the shell movements, the amplitude and the oscillation period make it possible to estimate the safety factor of the structure bearing capacity with non-destructive methods under operating conditions.

This article proposes the sumo-atclib framework, which provides a convenient uniform interface for testing adaptive control algorithms with different limitations, for example, restrictions on phase durations, phase sequences, restrictions on the minimum time between control actions, which uses the open source microscopic transport modeling environment SUMO. The framework shares the functionality of controllers (class TrafficController) and a monitoring and detection system (class StateObserver), which repeats the architecture of real traffic light objects and adaptive control systems and simplifies the testing of new algorithms, since combinations of different controllers and vehicle detection systems can be freely varied. Also, unlike most existing solutions, the road class Road has been added, which combines a set of lanes, this allows, for example, to determine the adjacency of regulated intersections, in cases when the number of lanes changes on the way from one intersection to another, and therefore the road graph is divided into several edges. At the same time, the algorithms themselves use the same interface and are abstracted from the specific parameters of the detectors, network topologies, that is, it is assumed that this solution will allow the transport engineer to test ready-made algorithms for a new scenario, without the need to adapt them to new conditions, which speeds up the development process of the control system, and reduces design overhead. At the moment, the package contains examples of MaxPressure algorithms and the Q-learning reinforcement learning method, the database of examples is also being updated. The framework also includes a set of SUMO scripts for testing algorithms, which includes both synthetic maps and well-verified SUMO scripts such as Cologne and Ingolstadt. In addition, the framework provides a set of automatically calculated metrics, such as total travel time, delay time, average speed; the framework also provides a ready-made example for visualization of metrics.

The article investigates the possibility of detecting traces of hazardous substances (explosives and narcotics) based on the detection of their vapors in the air. The relevance of the study stems from the need to counter terrorist threats and drug trafficking, where identifying even trace amounts of substances is critical. The focus is on mathematical modeling of the evaporation of a thin substance layer from a surface, based on molecular kinetic theory. A universal model is proposed, accounting for the physicochemical properties of substances, ambient temperature, adhesion to the surface, and the initial mass of the layer. Using the Hertz – Knudsen – Langmuir and Clausius – Clapeyron equations, analytical expressions are derived for the complete evaporation time, maximum vapor mass, and process dynamics. A dimensionless parameter, $\gamma$, is identified, determining the limiting conditions for evaporation. It is shown that substance adhesion (coefficient $\alpha$) affects the evaporation rate but not the final vapor mass. Calculations were performed for six model substances (TNT, RDX, PETN, amphetamine, cocaine, heroin) with a wide range of properties. At room temperature and a surface concentration of 100 ng/cm2, most substances evaporate completely, except for RDX, which remains on the surface at 84%. Evaporation times range from fractions of a second (amphetamine) to several hours (heroin). For low-volatility substances, the maximum mass capable of evaporating under given conditions is determined. The novelty of the work lies in the development of a universal model applicable to a broad class of hazardous substances and in identifying key parameters governing the evaporation process. The results enable the estimation of detection limits for trace substances using vapor-based methods and can be applied in the design of security systems.

The objective of this study is to determine the best formations for the joint movement of a group of small robots in an aquatic environment. Estimation of drag of the flow is a traditional and well-known area of research, but it is not always valid to extend the conclusions made for a single robot to a group of similar devices due to the physical effects that appear during joint movement, such as a wave shadow. For these reasons, it is necessary to study the hydrodynamic characteristics of certain robot formations as a stable structure. The hydrodynamic parameters of systems with two main types of propulsion were studied: locomotive (fishtails) and propellers. Formations similar in structure to schools of fish were mainly considered, and then their applicability for robots of different types was assessed. The relationship between the speed of movement of the group and the drag of each of its participants was also studied. Mathematical modeling of the flow around a group of robots was performed using the finite volume method using two software packages (FlowVision and OpenFoam). Robots with a screw propeller interfere with each other when packed into tight formations, and for the locomotive case, being in the disturbance zone, on the contrary, is preferable. Also, with poorly streamlined bodies, flows separating from the surface can turn into narrow turbulent jets that greatly interfere with the rear robots. It has been established that wake effect reduces energy costs only at low speeds of movement — about 5 cm/s; at high speeds, movement in columns becomes difficult for the rear robots. No large difference in frontal resistance was found between a single robot and a group for a fish-like tail. The studies made it possible to develop and substantiate recommendations for optimizing robot designs for group movement.

The paper presents a new dense material modeling method based on spherepolyhedra packing algorithm, describes mathematical model of spherepolyhedra and discuss the results of computation experiments on different spherepolyhedra packs. The results of experiments show convergence of proposed method. Experiments include investigations of spherepolyhedra packs with different shapes, polydisperse and oriented structures. Presented method would be applied to virtual design of dense materials composed of non-spherical particles.

A vector-matrix approach to the theoretical design of metabolic pathways converting chemical compounds, viz., preset substrates, into desirable products is described. It is a mathematical basis for computer–aided generation of alternative biochemical reaction sets executing the given substrate–product conversion. The pathways are retrieved from the used database of biochemical reactions and utilize the reaction stoichiometry and restrictions based on the irreversibility of a part of them. Particular attention is paid to the analysis of restriction interrelations. It is shown that the number of restrictions can be notably reduced due to the existence of families of parallel restricting planes in the space of reaction flows. Coinciding planes of contradirectional restrictions result in the existence of fixed reaction flow values. The problem of exclusion of so called futile cycles is also considered. Utilization of these factors allows essential lowering of the problem complexity and necessary computational resources. An example of alternative biochemical pathway computation for conversion of glucose and glycerol into succinic acid is given. It is found that for a preset “substrate–product” pair many pathways have the same high-energy bond balance.

Modern approach to modernization of the experimental techniques involves design of mathematical models of the wind-tunnel, which are also referred to as Electronic of Digital Wind-Tunnels. They are meant to supplement experimental data with computational analysis. Using Electronic Wind-Tunnels is supposed to provide accurate information on aerodynamic performance of an aircraft basing on a set of experimental data, to obtain agreement between data from different test facilities and perform comparison between computational results for flight conditions and data with the presence of support system and test section.

Completing this task requires some preliminary research, which involves extensive wind-tunnel testing as well as RANS-based computational research with the use of supercomputer technologies. At different stages of computational investigation one may have to model not only the aircraft itself but also the wind-tunnel test section and the model support system. Modelling such complex geometries will inevitably result in quite complex vertical and separated flows one will have to simulate. Another problem is that boundary layer transition is often present in wind-tunnel testing due to quite small model scales and therefore low Reynolds numbers.

In the current article the first stage of the Electronic Wind-Tunnel design program is covered. This stage involves computational investigation of aerodynamic characteristics of the generic flying-wing UAV model previously tested in TsAGI T-102 wind-tunnel. Since this stage is preliminary the model was simulated without taking test-section and support system geometry into account. The boundary layer was considered to be fully turbulent.

For the current research FlowVision computational code was used because of its automatic grid generation feature and stability of the solver when simulating complex flows. A two-equation k–ε turbulence model was used with special wall functions designed to properly capture flow separation. Computed lift force and drag force coefficients for different angles-of-attack were compared to the experimental data.

In the framework of modern non-equilibrium thermodynamics (macroscopic approach of description and mathematical modeling of the dynamics of real physical and chemical processes), the authors developed a potential- flow method for describing and mathematical modeling of real physical and chemical processes applicable in the general case of real macroscopic physicochemical systems. In accordance with the potential-flow method, the description and mathematical modeling of these processes consists in determining through the interaction potentials of the thermodynamic forces driving these processes and the kinetic matrix determined by the kinetic properties of the system in question, which in turn determine the dynamics of the course of physicochemical processes in this system under the influence of the thermodynamic forces in it. Knowing the thermodynamic forces and the kinetic matrix of the system, the rates of the flow of physicochemical processes in the system are determined, and according to these conservation laws the rates of change of its state coordinates are determined. It turns out in this way a closed system of equations of physical and chemical processes in the system. Knowing the interaction potentials in the system, the kinetic matrices of its simple subsystems (individual processes that are conjugate to each other and not conjugate with other processes), the coefficients entering into the conservation laws, the initial state of the system under consideration, external flows into the system, one can obtain a complete dynamics of physicochemical processes in the system. However, in the case of a complex physico-chemical system in which a large number of physicochemical processes take place, the dimension of the system of equations for these processes becomes appropriate. Hence, the problem arises of automating the formation of the described system of equations of the dynamics of physical and chemical processes in the system under consideration. In this article, we develop a library of software data types that implement a user-defined physicochemical system at the level of its design scheme (coordinates of the state of the system, energy degrees of freedom, physico-chemical processes, flowing, external flows and the relationship between these listed components) and algorithms references in these types of data, as well as calculation of the described system parameters. This library includes both program types of the calculation scheme of the user-defined physicochemical system, and program data types of the components of this design scheme (coordinates of the system state, energy degrees of freedom, physicochemical processes, flowing, external flows). The relationship between these components is carried out by reference (index) addressing. This significantly speeds up the calculation of the system characteristics, because faster access to data.

A new discrete ecological-evolutionary mathematical model is presented, in which the search mechanisms for evolutionarily stable migration routes of fish populations are implemented. The proposed adaptive designs have a small dimension, and therefore have high speed. This allows carrying out calculations on long-term perspective for an acceptable machine time. Both geometric approaches of nonlinear analysis and computer “asymptotic” methods were used in the study of stability. The migration dynamics of the fish population is described by a certain Markov matrix, which can change during evolution. The “basis” matrices are selected in the family of Markov matrices (of fixed dimension), which are used to generate migration routes of mutant. A promising direction of the evolution of the spatial behavior of fish is revealed for a given fishery and food supply, as a result of competition of the initial population with mutants. This model was applied to solve the problem of optimal catch for the long term, provided that the reservoir is divided into two parts, each of which has its own owner. Dynamic programming is used, based on the construction of the Bellman function, when solving optimization problems. A paradoxical strategy of “luring” was discovered, when one of the participants in the fishery temporarily reduces the catch in its water area. In this case, the migrating fish spends more time in this area (on condition of equal food supply). This route is evolutionarily fixes and does not change even after the resumption of fishing in the area. The second participant in the fishery can restore the status quo by applying “luring” to its part of the water area. Endless sequence of “luring” arises as a kind of game “giveaway”. A new effective concept has been introduced — the internal price of the fish population, depending on the zone of the reservoir. In fact, these prices are Bellman's private derivatives, and can be used as a tax on caught fish. In this case, the problem of long-term fishing is reduced to solving the problem of one-year optimization.

In this work we have developed a new efficient program for the numerical simulation of 3D global chemical transport on an adaptive finite-difference grid which allows us to concentrate grid points in the regions where flow variables sharply change and coarsen the grid in the regions of their smooth behavior, which significantly minimizes the grid size. We represent the adaptive grid with a combination of several dynamic (tree, linked list) and static (array) data structures. The dynamic data structures are used for a grid reconstruction, and the calculations of the flow variables are based on the static data structures. The introduction of the static data structures allows us to speed up the program by a factor of 2 in comparison with the conventional approach to the grid representation with only dynamic data structures.

We wrote and tested our program on a computer with 6 CPU cores. Using the computer microarchitecture simulator gem5, we estimated the scalability property of the program on a significantly greater number of cores (up to 32), using several models of a computer system with the design “computational cores – cache – main memory”. It has been shown that the microarchitecture of a computer system has a significant impact on the scalability property, i.e. the same program demonstrates different efficiency on different computer microarchitectures. For example, we have a speedup of 14.2 on a processor with 32 cores and 2 cache levels, but we have a speedup of 22.2 on a processor with 32 cores and 3 cache levels. The execution time of a program on a computer model in gem5 is 104–105 times greater than the execution time of the same program on a real computer and equals 1.5 hours for the most complex model.

Also in this work we describe how to configure gem5 and how to perform simulations with gem5 in the most optimal way.