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Dive into the research topics where A. I. Belousov is active.

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Featured researches published by A. I. Belousov.


Russian Aeronautics (iz Vuz) | 2009

On application of the theory of face seals with microgrooves to high-speed FV engine rotors

A. I. Belousov; S. V. Falaleev; A. S. Demura

With allowance made for thermoelasticity of working surfaces and inertia forces on the lubricant coat, a hydrodynamic problem is solved for the noncontacting face seals with microgrooves in the high-speed rotors of FV engines. Also shown are the initiation of surface waviness in the zone of lubricant coat fracture and the influence of its amplitude upon the seal characteristics.


Russian Aeronautics (iz Vuz) | 2014

Problems in formation and control of a required microacceleration level at spacecraft design, tests, and operation

A. I. Belousov; A. V. Sedel’nikov

In this paper, we consider the main aspects of a problem in formation and control of a required microacceleration level as the most important characteristic of the space laboratory intended for realizing the gravitational and sensitive technological processes. The estimation model and methodology to control and estimate the microaccelerations are presented that are necessary for the well-founded choice of the spacecraft parameters and carrying out their flight and space tests, when the new special-purpose space laboratories are designed and constructed.


Russian Aeronautics (iz Vuz) | 2007

Problems of application of face gasodynamic seals in aircraft engines

A. I. Belousov; S. V. Falaleev; A. S. Vinogradov; P. V. Bondarchuk

Problems arising in introduction of gasodynamic seals in aircraft engines are considered. The operation of a face gasodynamic seal as part of a natural gas pump is analyzed and its efficiency in the presence of oil is shown.


Russian Aeronautics (iz Vuz) | 2009

Theory of an annular corrugated damper in the vibrator precession motion

A. I. Belousov; Yu. K. Ponomarev; Yu. N. Pronichev; D. G. Krypaev

The theory for calculating elastodamping characteristics of multilayer corrugated dampers being used in the rotor supports of aircraft gas turbine engines (GTEs), turbo-pump assemblies of rocket engines as well as in different articles of machine building industry is presented.


Journal of Experimental and Theoretical Physics | 1999

Two-dimensional mesoscopic dusty plasma clusters: Structure and phase transitions

G. E. Astrakharchik; A. I. Belousov; Yu. E. Lozovik

A two-dimensional mesoscopic cluster of “dusty plasma” particles, which can be interpreted as a system of microparticles in an rf gas discharge, is investigated. The ground-state configurations and corresponding eigenfrequencies and eigenvectors are found for clusters of N=22–40 particles in a harmonic confining potential. It is shown that a change in the Debye screening length R of the particle charge in the plasma can cause structural transformations of the ground state of the system, manifested as first-order or second-order phase transitions with respect to the parameter R. The disorder (“melting”) of the clusters is analyzed in detail by Monte Carlo simulation and molecular dynamics. By varying the characteristic range of particle interaction in a cluster, it is possible to modulate its thermodynamic properties and the character of the phase transitions, thereby causing a controlled transition of the system into the fully ordered, orientationally disordered, or fully disordered state. The possibility of dusty plasma clusters coexisting in different states is discussed.


Jetp Letters | 1998

Quantum orientational melting and the phase diagram of a mesoscopic system

A. I. Belousov; Yu. E. Lozovik

The “phase diagram” of a two-dimensional mesoscopic system of bosons is investigated. An example of such a system is a system of indirect magnetoexcitons in semiconductor double quantum dots. Quantum Monte Carlo calculations show the existence of quantum orientational melting. At zero (quite low) temperature, as quantum fluctuations of the particles intensify, two quantum disordering phenomena occur with increasing de Boer parameter q. First, at q≈10−3 the system passes to a radially ordered but orientationally disordered state, where different shells of a cluster rotate relative to one another. Then at q≈0.16 a transition to a superfluid state occurs.


Solid State Communications | 1996

Topological phase transition in 2D quantum Josephson array

A. I. Belousov; Yu. E. Lozovik

Abstract Path Integral Quantum Monte Carlo simulation is used to study thermodynamic properties and a phase diagram of 2D quantum Josephson array, described by 2 + 1 XY model. The helicity and vorticity moduli, correlation function of phases and other characteristics of the system as functions of quantum parameter q and temperature T are studied ( q= h √JC ), J is the Josephson coupling constant, C is the intragrain capacitance). Quantum fluctuation induced superconductor-normal phase transition is studied in detail through the use of behavior of above-mentioned quantities. No discontinuous or reentrant phase transition in q-T plane is found. Analysis of the vorticity and the renormalized coupling constant leads to the conclusion that the whole line of phase transition is of Kosterlitz-Thouless type.


Russian Aeronautics (iz Vuz) | 2013

Probabilistic estimation of fulfilling favorable conditions to realize the gravity-sensitive processes aboard a space laboratory

A. I. Belousov; A. V. Sedel’nikov

We consider a probabilistic estimation of microaccelerations being produced in the inboard environment of an orbital laboratory as a random process; based on this estimation we analyzed a probability of fulfilling the favorable conditions to realize gravity-sensitive processes. The approach suggested can be applied when designing a space laboratory to meet the requirements for the microaccelerations inside the working zone of technological equipment.


Russian Aeronautics (iz Vuz) | 2015

Synthesis of basic structural design of aircraft GTE based on genetic algorithms

A. I. Belousov; A. Yu. Sapozhnikov

A functional IDEF0-model of conceptual design of an aircraft gas turbine engine was developed. By an example of selecting a structural design of two-rotor gas turbine engine, we present the structured analysis of the engine and describe the operation of the genetic algorithm.


Russian Aeronautics (iz Vuz) | 2014

Methodology of modernizing the serial converted gas turbine unit

A. I. Belousov; S. V. Nazdrachev

The ways and special features of modernizing the ground-based power plants that are converted from the aircraft gas turbine engines as well as the appearing problems are considered by an example of the NK family engines being developed.

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Yu. E. Lozovik

Russian Academy of Sciences

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S. A. Verzakov

Russian Academy of Sciences

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G. E. Astrakharchik

Polytechnic University of Catalonia

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S. A. Berzakov

Russian Academy of Sciences

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