SIBERIAN JOURNAL OF PHYSICS. Scientific Journal. 2018. V13, i 1

Radiophysics and Electronics

Budnikov K. I., Kurochkin A. V. Method of Experimental Research of HTTP Filters

Filtering of user requests to Internet resources allows regulating access to the information requested. The paper presents a technique for bench testing of characteristics of the HTTP protocol filtering device, which includes the scheme and procedure of testing, the method of obtaining and evaluating the properties of the device under study. A two-channel symmetric computer model of the HTTP request filter is considered. It operates at the packet level, using the method of restricting access to the Internet resource by its URL. The results of experimental tests of the model according to the proposed technique are presented.

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High-Energy and Accelerator Physics, Physics of High-Temperature Plasma

Arzhannikov A. V., Kalinin P. V., Sandalov E. S., Sinitsky S. L. Selective Properties of a Planar Electrodynamic System for Two-Stage Generation of Terahertz Radiation

The paper presents the results of computer 3D-modeling and «cold» measurements of the selective properties, obtained for the main units of the planar electrodynamic system that is intended for the two-stage generation of terahertz radiation. During the investigations, the calculated and measured values characterizing these properties, were compared in order to search for the optimal geometry of the electrodynamic system units. The performed optimization should ensure the achievement of a high level of power and coherence both at the first stage, when mm-radiation is generated, and at the second stage, when it is converted to the terahertz band through scattering by an electron beam.

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Physics of a Fluid, Neutral and Ionized Gases

Lysenko V. I., Gaponov S. A., Zubkov N. N., Smorodsky B. V., Ermolaev Yu. G., Kosinov A. D. Influence of Dispersed Tangential Heavy-Gas Blowing into the Supersonic Boundary- Layer on Its Stability

Joint theoretical and experimental investigation of the influence of the distributed tangential blowing (into a boundary layer) heavy gas (sulfur hexafluoride of SF6) on hydrodynamic stability to natural disturbances of the supersonic flat-plate boundary layer at free-stream Mach number M = 2 have been performed. For the first time experimentally it is shown that in case of such blowing there is a boundary-layer stabilization, generally due to reduction of growth of disturbances at higher frequencies. At the same time the frequency corresponding to the maximum spatial disturbance amplification rates decreases.

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Kornilov V. I. Steady Blowing / Suction into Turbulent Boundary Layer of a Symmetrical Aerofoil Section

The efficiency of steady air blowing / suction into the turbulent boundary layer of the NACA 0012 aerofoil section in an incompressible flow was studied experimentally. The blowing / suction was carried out through finely perforated sections located on the adjacent sides of the wing and being parts of its streamlined surface. The studies were performed at the Reynolds number Rec = 0.7x10^6 in the range of angles of attack a = –6 – 6?. The obtained results clearly indicate the ambiguous nature of the combined control action in the form of blowing / suction on the aerofoil aerodynamic characteristics. The maximum gain in lift-to-drag ratio of about 1.8 units is achieved at zero angle of attack a. An increase in a leads to a decrease in the effectiveness of this method of action on the boundary layer.

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Ivashchenko V. A., Mullyadzhanov R. I. Numerical Simulation of Stratified Submerged Jet

ÈIn this paper, stratified jet flows are investigated using the numerical simulation method. For a high accuracy of spatial discretization of the Navier-Stokes equations the method of spectral elements was chosen. By the method of direct numerical simulation (DNS) the solution algorithm was validated using the example of a turbulent flow in a periodic pipe with Reynolds number Re = 5 300, constructed using the average velocity and the diameter of the pipe. Comparison of statistical characteristics showed good agreement with the literature data. A further investigation was concentrated on a circular turbulent air jet flowing into a space filled with air, helium or carbon dioxide. For the air-to-air pair, the results are shown to be in good agreement with the literature data and other LES calculations. During the analysis of the helium-air and carbon dioxide-air pairs, their basic similarities and differences were revealed both with each other and with the air-air pair, it was suggested that the effects associated with stratification predominate over viscous effects.

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Shmakov A. G., Vikhorev V. V., Grek G. R., Kozlov V. V., Kozlov G. V., Litvinenko Yu. A. Combustion of the Round Microjet Premixed Hydrogen with Oxygen Efflux from the Linear Channel

The purpose of this work consists in experimental study of combustion features of the round microjet premixed hydrogen with oxygen. Situation of the microjet efflux and combustion of hydrogen/ oxygen mixture from a straight micronozzle with a parabolic mean velocity profile at the nozzle exit is considered. It is shown that addition of oxygen leads to decrease in velocity range of existence of a microjet combustion in comparison with similar parameter at diffusion combustion of a pure hydrogen. It is found that with growth of a microjet velocity efflux, the combustion termination of its is connected with reduction of an oxygen part in mixture. It is revealed that the spherical shape of «bottleneck flame region» is transformed to the narrow and extended area of a laminar flame of a cylindrical shape. Its thinning process grows with growth of microjet velocity efflux.

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Vikhorev V. V., Grek G. R., Kozlov V. V., Litvinenko Yu. A., Litvinenko M. V., Shmakov A. G. Combustion of the Round Microjet of Hydrogen with Oxygen Mixture Efflux from the Curved Micronozzle

The purpose of this work consists in experimental study of combustion features of the round microjet premixed hydrogen with oxygen. Situation of the microjet efflux and combustion of hydrogen/ oxygen mixture from a curved micronozzle with a top-hat mean velocity profile at the nozzle exit is considered. It is shown that addition of oxygen leads to decrease in velocity range of existence of a microjet combustion in comparison with similar parameter at diffusion combustion of a pure hydrogen. It is found that with growth of a microjet velocity efflux, the combustion termination of its is connected with reduction of an oxygen part in mixture. Existence of spherical «bottleneck flame region» is revealed. Its region deformed under influence of the Dean and Kelvin – Helmholtz vortices. «Bottleneck flame region» size is reduced with growth of a microjet velocity efflux. It is shown that the area of a turbulent flame is also is subjected to distortion from influence of the Dean and Kelvin – Helmholtz vortices. It is found that the range of the round microjet combustion both pure hydrogen, and its mixture with oxygen efflux from a curved micronozzle is much wider than the range of the round microjet combustion both pure hydrogen, and its mixture with oxygen efflux from a linear micronozzle.

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Korobeishchikov N. G., Roenko M. A., Nikolaev I. V. Diagnostics of Gas Cluster Flows by Transverse Intensity Profile of Molecular Beam

An experimental method for diagnostics of clusters in molecular beams formed from supersonic gas jets is described. The method is based on measuring the cross-section profile of the mass intensity of the beam at a given distance behind the skimmer and it allows one to determine the main parameters: the mean cluster size, the ratio of clusters to monomers and the cluster flow density. The described method can be used to diagnose cluster beams of any pure gases, without creating special models or determining empirical constants. Since the cluster beam has a high intensity, highly sensitive and complex equipment is not required for measurements. With this method, the average sizes of Ar clusters in the range from 50 to 2,000 molecules per cluster were determined. The reliability of the obtained values of the mean cluster sizes is confirmed by a comparison of the results with the data of other authors obtained by the various experimental methods using the similarity parameter of flows with condensation (the Hagena parameter) Ã*. The physical limitations of the described method were analyzed.

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Prokhorov E. S. Computation of Equilibrium States of Reacting Carbon-Oxygen Thermodynamic System

The problem of determining the equilibrium states of reacting thermodynamic system that is the molecules of substances consisting of only oxygen and carbon atoms has been numerically solved basing on given external parameters (pressure and temperature). Here it has been assumed that the shift of system chemical equilibrium resulting from the chemical reaction can imply the presence of condensed carbon as suspended ultradispersed graphite particles among the gaseous products of reaction. In computations, the values of pressure, temperature and the relation of concentration of oxygen and carbon atoms have been varied. The conditions, under which carbon condensate appears in the reaction products and homogeneous thermodynamic system becomes heterogeneous one, have been determined.

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Solid-State and Semiconductor Physics, Physics of Nanostructures

Kovalyov A. A. Generation Lines Selector for Molecular IR Lasers

Applicability of several approaches to generation lines selection in molecular IR laser is investigated: diffraction grating placed in spite of one of cavity mirrors, Bragg mirror, inclined and reflective interferometers. A selector is proposed which combines advantages of Michelson interferometer with phase reflective interferometer, and which permits reliable selection of a chosen vibrationrotation generation line. The selector calculation is performed for the case of waveguide CO2 laser. Two variants of schemes for laser tunability over generation lines are analyzed by using this selector.

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