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В работе проведен расчет 1/2-волнового преобразователя продольных ультразвуковых колебаний и волнового преобразователя продольно-крутильных ультразвуковых колебаний методом конечных элементов в среде программного пакета Abaqus. В результате расчета определены размеры концентратора продольно-крутильных колебаний и частотно-амплитудные характеристики преобразователей продольных и продольно-крутильных колебаний. Наложение продольно-крутильных колебаний на инструмент в процессах поверхностно-упрочняющей обработки деталей из титановых сплавов позволит уменьшить адгезионную составляющую трения в зоне контакта. Проведено сравнение результатов конечноэлементного расчета частотно-амплитудных характеристик преобразователей с экспериментальными данными, погрешность расчета не превышает 2.5 %.

In this study the calculation of 1/2-wave transducer of longitudinal ultrasonic oscillations and one wave transducer of longitudinal-torsion ultrasonic oscillations were carried out by finite element method with use of Abaqus. Dimensions of the concentrator of longitudinal-torsional oscillations and frequency-amplitude characteristics of the transducers of longitudinal and longitudinal-torsional oscillations were defined by calculation. Application of ultrasonic longitudinal-torsional oscillations at tool during surface-strengthening treatment of details made of titanium will allow to reduce adhesion portion of friction in the contact zone. A comparison of results of finite-element calculation of frequency-amplitude characteristics with experimental ones were made and calculation error does not exceed 2.5 %.

This paper studies electromagnetic fields, frequencies of lasing, and emission thresholds of a drop-shaped microcavity laser. From the mathematical point of view, the original problem is a nonstandard two-parametric eigenvalue problem for the Helmholtz equation on the whole plane. The desired positive parameters are the lasing frequency and the threshold gain, the corresponding eigenfunctions are the amplitudes of the lasing modes. This problem is usually referred to as the lasing eigenvalue problem. In this study, spectral characteristics are calculated numerically, by solving the lasing eigenvalue problem on the basis of the set of Muller boundary integral equations, which is approximated by the Nystr¨om method. The Muller equations have weakly singular kernels, hence the corresponding operator is Fredholm with zero index. The Nyström method is a special modification of the polynomial quadrature method for boundary integral equations with weakly singular kernels. This algorithm is accurate for functions that are well approximated by trigonometric polynomials, for example, for eigenmodes of resonators with smooth boundaries. This approach leads to a characteristic equation for mode frequencies and lasing thresholds. It is a nonlinear algebraic eigenvalue problem, which is solved numerically by the residual inverse iteration method. In this paper, this technique is extended to the numerical modeling of microcavity lasers having a more complicated form. In contrast to the microcavity lasers with smooth contours, which were previously investigated by the Nyström method, the drop has a corner. We propose a special modification of the Nyström method for contours with corners, which takes also the symmetry of the resonator into account. The results of numerical experiments presented in the paper demonstrate the practical effectiveness of the proposed algorithm.

This paper studies electromagnetic fields, frequencies of lasing, and emission thresholds of a drop-shaped microcavity laser. From the mathematical point of view, the original problem is a nonstandard two-parametric eigenvalue problem for the Helmholtz equation on the whole plane. The desired positive parameters are the lasing frequency and the threshold gain, the corresponding eigenfunctions are the amplitudes of the lasing modes. This problem is usually referred to as the lasing eigenvalue problem. In this study, spectral characteristics are calculated numerically, by solving the lasing eigenvalue problem on the basis of the set of Muller boundary integral equations, which is approximated by the Nystr¨om method. The Muller equations have weakly singular kernels, hence the corresponding operator is Fredholm with zero index. The Nyström method is a special modification of the polynomial quadrature method for boundary integral equations with weakly singular kernels. This algorithm is accurate for functions that are well approximated by trigonometric polynomials, for example, for eigenmodes of resonators with smooth boundaries. This approach leads to a characteristic equation for mode frequencies and lasing thresholds. It is a nonlinear algebraic eigenvalue problem, which is solved numerically by the residual inverse iteration method. In this paper, this technique is extended to the numerical modeling of microcavity lasers having a more complicated form. In contrast to the microcavity lasers with smooth contours, which were previously investigated by the Nyström method, the drop has a corner. We propose a special modification of the Nyström method for contours with corners, which takes also the symmetry of the resonator into account. The results of numerical experiments presented in the paper demonstrate the practical effectiveness of the proposed algorithm.

В последние несколько лет наблюдаются значительные успехи в области создания двигательных установок для летательных аппаратов, основанных на сжигании топлива во вращающейся детонационной волне. В научных лабораторияхпо всему миру проводятся как фундаментальные исследования, связанные, например, с вопросами смесеобразования при раздельной подаче топлива и окислителя, так и прикладные по доводке уже существующих прототипов. В работе приводится краткий обзор основных результатов наиболее значимых недавних расчетных работ по изучению распространения одномерной пульсирующей волны газовой детонации в среде с неравномерным распределением параметров. Отмечаются общие тенденции, которые наблюдали авторы данных работ. В этих работах показано, что наличие возмущений параметров перед фронтом волны может приводить к регуляризации и к резонансному усилению пульсаций параметров за ее фронтом. В результате возникает привлекательная с практической точки зрения возможность влиять на устойчивость детонационной волны и управлять ею. Настоящая работа направлена на создание инструмента, который позволяет изучать газодинамические механизмы данных эффектов.

Математическая модель основана на одномерных уравнениях Эйлера, дополненных одностадийной моделью кинетики химических реакций. Определяющая система уравнений записана в системе координат, связанной с лидирующим скачком, что приводит к необходимости добавить уравнение для скорости лидирующей волны. Предложен способ интегрирования данного уравнения, учитывающий изменение плотности среды перед фронтом волны. Таким образом, предложен вычислительный алгоритм для моделирования распространения детонации в неоднородной среде.

С использованием разработанного алгоритма проведено численное исследование распространения устойчивой детонации в среде с переменной плотностью. Исследован режим с относительно небольшой амплитудой колебаний плотности, при котором колебания параметров за фронтом детонационной волны происходят с частотой колебаний плотности среды. Показана связь периода колебаний параметров со временем прохождения характеристик C₊ и C₀ по области, которую условно можно считать зоной индукции. Сдвиг по фазе между колебаниями скорости детонационной волны и плотности газа перед волной оценен как максимальное время прохождения характеристики C₊ по зоне индукции.

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.