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Abstract
Citation: Valentin A. Tenenev. On the Occasion of his 75th Birthday, Rus. J. Nonlin. Dyn., 2024, Vol. 20, no. 3, pp. 339-343
DOI:10.20537/nd241001
Koroleva M. R.,  Tenenev V. A.
Abstract
Three methods for constructing an approximate Riemann solver for the Soave – Redlich – Kwong real gas model are presented: linearization of nonlinear equations, cubic interpolation, and local approximation of the equation of state by a two-term equation of state. These methods are tested by considering the problem of the decay of a discontinuity in a pipe in an axisymmetric setting for the low-molecular and high-molecular substances, including a region of nonclassical gas behavior. It is demonstrated that the linearization method is reasonable only for the testing problems. The method of approximation by cubic splines is acceptable for complex three-dimensional nonstationary calculations. However, it is found that the bicubic interpolation method does not work well for flows with large pressure drops. The local approximation method is the most economical and universal for practical calculations. It has been used for numerical modeling of real gas flows through a safety valve. The results of calculations for hydrogen and water vapor in a wide range of pressure variation are presented. The method of local approximation of the equation of state allows one to describe all features of gas flows for complex problems.
Keywords: Riemann problem, Godunov method, approximate solver, Soave – Redlich – Kwong equation of state
Citation: Koroleva M. R.,  Tenenev V. A., Approximate Riemann Solvers for the Soave – Redlich – Kwong Equation of State, Rus. J. Nonlin. Dyn., 2024, Vol. 20, no. 3, pp. 345-359
DOI:10.20537/nd240905
Lipanov A. M.,  Karskanov S. A.
Abstract
The results of the theoretical solution of the problem of braking a supersonic flow in a round pipe based on direct numerical simulation by integrating the Navier – Stokes equations without the use of additional models and empirical constants are shown. Shaded maps of density distribution depending on flow parameters are presented. The flow consists of successive rhombus-shaped shock waves distributed along the entire length of the channel. It is determined that the size of x-shaped structures depends on the flow parameters. At a lower Mach number, the rhombuses have a smaller size and, accordingly, their number increases along the length of the channel. The Reynolds number also affects the size of structures, however, it is less pronounced. With a lower Reynolds number, x-shaped structures have a smaller size. It is shown that over time the flow tends to a stationary state.
Keywords: direct numerical simulation, Navier – Stokes equations, supersonic flows, highorder approximation, Reynolds number, Mach number
Citation: Lipanov A. M.,  Karskanov S. A., Direct Numerical Simulation of Supersonic Gas Flow Through a Circular Cylindrical Channel, Rus. J. Nonlin. Dyn., 2024, Vol. 20, no. 3, pp. 361-369
DOI:10.20537/nd240803
Lipanov A. M.,  Shumikhin A. A.,  Karpov A. I.
Abstract
The ignition of a fuel pellet in a gas generator chamber is a time-consuming complex physicochemical process. During the ignition of the checker, the operating conditions of the device differ significantly from the conditions of its operation in the main area of operation. In particular, an important characteristic of the initial stage is the pattern of flame propagation over the surface of the fuel. A computational algorithm for modeling unsteady turbulent flows of compressible viscous gas based on numerical integration of unsteady equations obtained using physical conservation laws was used to study the vortex flow of gas in the gas generator path and the ignition process of the fuel block. The method used a system of equations written in a cylindrical coordinate system. The computational algorithm is based on a modified flow vector splitting scheme (Steger – Warming scheme). The algorithm has the 2nd order of accuracy in space. The obtained results of numerical simulation of the gas flow in the gas generator allow us to investigate the patterns of development of the ignition process of the fuel block in time, depending on the nature of the gas flow in the combustion chamber.
Keywords: vortex flow, large eddy simulation, turbulence, computational fluid dynamics
Citation: Lipanov A. M.,  Shumikhin A. A.,  Karpov A. I., Numerical Studies of the Influence of the Nature of the In-Chamber Flow on the Initial Period of Operation of the Gas Generator, Rus. J. Nonlin. Dyn., 2024, Vol. 20, no. 3, pp. 371-384
DOI:10.20537/nd240903
Koroleva M. R.,  Mishchenkova O. V.,  Chernova A. A.
Abstract
This paper presents a survey of original methods for solving problems of current interest concerning numerical simulation of the dynamics of operation of a direct-acting relief valve, as formulated and tested by Professor V.A. Tenenev, Doctor of Physics and Mathematics. New methods (not based on experimental data) are proposed to solve the problem of selecting an initial clearance and initial conditions for the dynamic characteristics of disk motion in a spring-loaded relief valve. A method due to V.A. Tenenev for constructing a computational dynamical grid for a three-dimensional analysis of the complete cycle of valve operation (“open-closed”) is presented. Approaches and methods for reducing the dimensionality of the problem of operation of the relief valve are discussed. Methods of taking into account the influence of the gas-dynamic feedback on the working processes in relief valves are developed and presented. Methods, numerical schemes and algorithms for taking into account the real properties of substances in simulating the operation of the valve are presented.
Keywords: numerical simulation, spring-loaded direct-acting relief valve, gas dynamics, operation of the relief valve, computational schemes and algorithms
Citation: Koroleva M. R.,  Mishchenkova O. V.,  Chernova A. A., Original Methods and Approaches to Numerical Simulation of Physical Processes in Fast-Response Technical Systems, Rus. J. Nonlin. Dyn., 2024, Vol. 20, no. 3, pp. 385-411
DOI:10.20537/nd240901
Korepanov M. A.,  Koroleva M. R.,  Mitrukova E. A.,  Nechay A. N.
Abstract
The formation of a supersonic gas target for lasers that operate in the extreme ultraviolet wavelengths is considered. The gas target is generated in the interaction zone of two opposite supersonic gas jets. The emission properties of inert gas targets were investigated experimentally. The distributions of the emission radiation intensity for argon, krypton and carbon dioxide were obtained and the shapes of the emission zone were detected.
The experimental conditions were reproduced in numerical experiments. The mathematical model of viscous compressible gas was used to model the gas dynamics of supersonic gas jets. The problem was solved in a two-dimensional axisymmetric setting for argon. The obtained distributions of the main gasdynamic quantities made it possible to detail the flow features and estimate the size of the emission zone, as well as the density level corresponding to this zone. It was demonstrated that the results of calculations qualitatively agree with the experimental data. In addition, it was found that the density level of the emission region with the required extreme ultraviolet intensity factor can be obtained by monitoring the total pressure.
Keywords: extreme ultraviolet laser, gas target, argon, experiment, mathematical modeling, opposite supersonic nozzles
Citation: Korepanov M. A.,  Koroleva M. R.,  Mitrukova E. A.,  Nechay A. N., Mathematical Modeling of the Gas-Jet Target for Extreme Ultraviolet Laser, Rus. J. Nonlin. Dyn., 2024, Vol. 20, no. 3, pp. 413-424
DOI:10.20537/nd240904