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Authors
Development of the numerical differentiation method for approximating pitch acceleration using sensor fusion approach
Korsun O.N., Goro S., Om M.H.
Recurrent matrix form of the optimal elimination method
Zhdanov A.I., Yablokova L.V.
Technological processes simulation incomplex parts production of aerospacetechnical equipment: problems and the ways of their solving
Bolotov M.A., Zhidyaev A.N., Surkov O.S.
Method of singular integral equations (SIE) in theory of dish antennas
1 1., 1 1., 1 1.
Applying Lagrange’s approach to solving a one-dimensional problem of wave propagation in gas in linear formulation
Nikonov V.V., Shakhov V.G.
Development of a model for determination of preloads on blade shrouds
Pechenina E.Y., Kudashov E.V., Pechenin V.A.
Comparative research of algorithms of measuring the geometry of complex profiles of gas turbine engine compressor blades
Pechenin V.A., Bolotov M.A., Ruzanov N.V., Stepanova E.R.
The effect of the way of setting boundary conditions on the results of modeling a flow at the flameholder outlet
Kolomzarov O.V., Anisimov V.M., Zubrilin I.A.
Optical characteristics of a multilayer solar sail and their effect on its heliocentric motion
Rozhkov M.A.
Substantiation of the criteria for evaluation of the efficiency of the fuel supply system of the gas turbine engines
Smurova N.A.
Topology optimization of a load-bearing structure via the method of convex linearization
Kishov E.A., Komarov V.A.
Doppler method for measuring fluctuations of elements rotationg parts power
Danilin A.I., Gretskov A.A.
Models and methods of optimizing the procedure of measuring gas turbine engine parts using coordinate measuring devices
Bolotov M.A., Lyozin I.A.
Parametric function of differential backscattering in multiple scattered media
Zakharov V.P., Sindyaeva A.R.
Method of orthotransformation of space images in conditions of lack of cue
Spirin A.V., Rudnev N.I., Pastuh N.K., Shuklin I.I.
Modeling non-through surface cracks in the thin-walled structures
Skvortsov Y.V., Glushkov S.V.
Optimal stabilization of small spacecraft angular motion in the process of deployment of an orbital tether system
Zabolotnov Y.M., Lobankov A.A.
Identification of scale factor of a pendulum compensating accelerometer during an orbital spacecraft mission
Fominov I.V.
Mathematical model of anisotropic elastic-plastic material
Grechnikov F.V., Yerisov Y.A.
Solving the polynomial approximation problem with use of the iterative kachmazh method
Ivanov A.A.
Investigation of the edge effect in composites using the ANSYS software in a two-dimensional formulation
Skvortsov Y.V., Evtushenko M.A.
Implementation of FDTD-method by means of CUDA-technology
Golovashkin D.L., Malysheva S.A.
Features of calculation of hydraulic characteristics of capillary spray jets of is liquid-stnyh rocket engines of small pull-rod
1 1., 1 1., 1 1.
Developing an electronic reference book on thermogasodynamic properties of rocket engine fuel combustion products taking into account non-ideal character of the working process
Silyutin M.V.
Solving the least squares problem using the method of an extended set of equations with sparse matrix
Gogoleva S.Y., Zoteeva O.V.
Computer-aided-design system for calculating adsorption thermodynamic characteristics
Zelenko L.S., Varfolomeyeva V.V., Kuznetsov V.Y., Fed’kayev A.V., Terentyev A.V., Buryak A.K.
Optimal design of an induction heater of minimum length
Mednikova V.A.
Disturbed transatmospheric motion of the first stage of an aerospace system
Krikunov M.M.
Transducer of fluid and air consumption and temperature in pipelines
Nikolayev V.N., Kabanov Y.N.
Method of design calculation gas-liquid jet duplex fuel nozzle with internal mixing
Egorychev V.S.
Backstepping synthesis of the height control system of an unmanned aerial vehicle
Akhramovich S.A., Barinov A.V., Malyshev V.V., Starkov A.V.
Prospective lines of improving the process of evaluating the technical condition of aircraft hydraulic system working fluid
Koptev A.N., Gareyev A.M., Popelnyuk I.A.
Methods of organization and evaluation of the results of planning economic activity of industrial enterprises based on IPF-technologies
Khaytbaev V.A., Nemchinov O.A.
Dimensions of controlled on CMM flat surfaces as an influencing factor of their coordinate-positional parameters measurement errors
Cheveleva A.O., Bolotov M.A.
Numerical simulation of separation processes in mechanical working
Ivanov K.M., Vinnik P.M., Ivanov V.N.
Features computer simulation cluster charactiristics electromagnetic converters
Merkulov A.I., Lavrov A.Y., Burkov D.S.
Analysis of the applicability of laser stereolithography technology for the production of turbodrives
Shabliy L.S.
Design of led spotlight secondary optics producing required irradiance distribution
Belousov A.A., Moiseev M.A.
Analysis of the structure of the third variation of roll moment coefficient during hypersonic flow about bodies of revolution with small spatial surface variations on the basis of differential locality hypothesis method
Danilkin V.A., Kostin G.F., Mokin Y.A., Tikhonov N.N.
Decrease in toxicity of transport diesel engines by neutralisation nitrogen oxide of the fulfilled gases
1 q., 1 1.
A parallel algorithm in the cyclic counter-sweep method for a two-dimensional domain
Loganova L.V.
Rectangular cantilever plate bending with regard to transverse shear deformation
Sukhoterin M.V.
Experimental research of wall boundary flow formation in the combustion chamber of a small gas generator with self-igniting fuel components
Shustov S.A.
Properties of a multi-layer multi-span corrugated package
Alkeev R.I., Suslikov V.I., Eskin I.D.
Development of numerical models of working process in fuel auger-centrifugal pump
Gafurov S.A., Miheev M.G., Rodionov L.V., Kruchkov A.N., Shahmatov E.V.
Analysis of information characteristics of a dynamic displacement doppler transducer signal
Danilin A.I., Gretskov A.A.
Calculation of the performance of a coulomb friction damper of a crown bevel gear wheel for different forms of resonant oscillations
Kozharinov E.V., Temis J.M.
Calculation of displacements in a viscoelastic square plate with a round cut
Ivanov E.Y.
Algorithm of planning operational and financial activity of a manufacturing enterprise
Bogatyryov V.D., Yesipova O.V.
Methods of protecting unpressurized compartments of spacecraft from the penetration of electromagnetic field
Syomkin N.D., Balakin V.L., Bragin V.V.
Structure of arterial blood pressure monitors
Fedotov A.A., Akulov S.A., Akulova A.S.
Analysis and assessment of efficiency of measures to stabilise the situation in the mortgage market
Kirillov A.V., Korostlyova T.S.
Analytical approximation of aircraft dynamics model in problems of approximate optimal control synthesis
Blinov A.O., Gurman V.I., Fralenko V.P.
Research of roughness of surface rollers with modified contact on the basis of analysis of thear autocorrelation functions
Nosov N.V., Abramov A.D., Haustov V.I.
Criteria of discrete phase control of blade working condition and their feasibility in systems of turbine driven set automatic control
Danilin A.I., Tchernyavsky A.Z.
Method of calculating currents of a group of parallel electric arc steel melting furnaces
Saltykov A.V.
Method of calculating self-capacitance in planar structural elements of a spacecraft
Syomkin N.D., Bragin V.V., Pomelnikov R.A., Balakin V.L.
Application of acoustic emission and scleroscopy for the analysis of carbon fiber-reinforced plastic samples with different degrees of matrix curing
Veshkin Е.A., Istyagin S.E., Kirilin S.G., Semenychev V.V.
Cyclic compression of a multi-layer multi-span corrugated package with plastic deformation of its tapes
Alkeev R.I., Suslikov V.I., Eskin I.D.
Application of contactless measuring complex «ARAMIS» in experimental tasks
Lezhin D.S., Parovay F.V., Sobul A.V.
Disturbed motion of a hypersonic vehicle in climb
Balakin V.L., Krikunov M.M.
Metrological analysis of a device rof nondestructive control of flight vehicle fuel tank current conductive coatings
Samsonov A.S., Blinov D.I., Skvortsov B.V., Zhivonosnovskaya D.M.
Dynamic modelling of non-linear vibrations in cylindrical tooth gearing of aircraft drive systems
Kalinin D.V., Temis J.M.
Improving the accuracy of assessing the position deviation in coordinate measurements of GTE compressor and turbine blade profiles
Bolotov M.A., Pechenin V.A., Ruzanov N.V.
Use of differential equations in the form of Encke for the study of motion small solar system bodies
Zausaev D.A.
NC machine tools contact measuring devices uncertainty when products geometrical parameters control
Bolotov M.I., Zhidyaev A.N., Surkov O.S., Tiapaev N.V., Papsuev I.V.
Design procedure of factor of rigidity of aviation elastic elements
Barmanov I.S.
Primary converters for the implementation of Doppler method for measuring blade oscillation power unit
Danilin A.I., Gretskov A.A.
Research of errors of measuring angular location parameters of holes in turbine and compressor discs of gas turbine engines
Bolotov M.A., Zhidyaev A.N., Shitarev I.L., Cheveleva A.O.
Processing of experimental data by the method of the least squares
1 1., 1 1., 1 1.
Research and rationing admissible nick on working blades of the compressor for engine NK-12 example
1 1., 1 1., 1 1., 1 1.
Formation of a structural calculated mesh the passage blade of the axial turbine in program GAMBIT
Baturin N.V., Baturin O.V., Matveev V.N.
Identification and procedure of reducing periodic noise of internal combustion car engines using the active compensation method
Vasilyev A.V., Andreyev S.S., Butsayev I.V., Pimkin V.V.
Germanuim monocrystals growing system based on contact method of measurement
Sahanski S.P.
Choosing the form of space vehicle designed for descent in the rarefied atmosphere of Mars
Aslanov V.S., Ledkov A.S.
Limit values of the Brayton cycle with the use of reduced fuel characteristics
Mikheenkov E.L., Nekrasova S.O.
Three-dimensional periodic thermoelastichydrodynamic modeling of hydrodynamic processes of a thrust bearing
Sokolov N.V., Khadiev M.B., Fedotov P.E., Fedotov E.M.
Method for optimizing mass and size characteristics of a high-pressure turbine disk
Siluyanova M.V., Grunin A.N., Alendar A.D., Kandaurov S.K.
Analysis of control programs and climb paths of the hypersonic first stage of an aerospace system
Balakin V.L., Krikunov M.M.
Protocols of stitching image strips formed by optoelectronic converters and their application
Kuznetsov P.K., Martem’ianov B.V., Miatov G.N., Yudakov A.A.
Analysis of motion stability of a deployed space tether system with an atmospheric probe
Zhe D., Zabolotnov Y.M., Changqing W.
Primary assessment of the effects of temperature drop on the mechanical properties of a protective oxide layer obtained by microarc oxidation on alloy AK9
Krishtal M.M., Ivashin P.V., Pavlov D.A., Polunin A.V.
Mathematic simulation of AL-31F powerplant radiation in the IR range
Filippov G.S.
The device for the determination of blades oscillation parameters based on nonlinear approximation of primary transducers signals
Danilin A.I., Chernyavskiy A.Z., Danilin S.A.
Automated generation of structural members of a spacecraft thermal model
Kulikov D.S., Shatin A.A., Velmisov I.G.
Calculation of cutting temperature at milling of purveyances from hard-processing materials
Trusov V.N., Skuratov D.L., Zakonov O.I., Shikin V.V.
Optimum programs of correction of quasielliptical and circular orbits of spacecraft with the limited-thrust engine
Khramov A.A.
Improving the operating characteristics of engines by the imposition of manufacturing operation of hermeticity inspection of vacuum-tight radio electronic device cases
Features of the new gas turbine aviation engines theory course
Mingazov B.G., Kosterin V.A., Varsegov V.L.
The devices for the diagnosis and control of turbine blades deformative condition during operation
Danilin A.I., Chernyavskiy A.G., Kapustin A.S.
Use of control volume method for the temperature field calculation by laser influence
Murzin S.P., Mezhenin A.V., Osetrov E.L.
Calculation of spatial distribution of energy of a complex radiator
Yevdokimov I.Y., Nikolaenko V.S., Filippov G.S., Yashchenko B.Y.
Method of reduced fuel characteristics and parameters of the operating cycles of heat engines
Anastaseev V.V., Belozertsev S.V., Mikheenkov E.L., Nekrasova S.O.
Application of gas analyzers for the control of fuel in the air environment of rocket and space industry enterprises
Bulgakov A.B., Vashchuk S.P., Panshin R.A.
Disturbed motion of the hypersonic first stage of an aerospace system in climb
Balakin V.L., Krikunov M.M.
The concept of generalized method of calculation and design of wet cleaning duct GTD
Silaev B.M., Malcev E.N.
Analysis of control programs and flight paths of a hypersonic vehicle in climb
Balakin V.L., Krikunov M.M.
Experimental study of a method of reducing the drag of a circular cylinder by installing a flat plate
Frolov V.A., Kozlova A.S.
Application of simulation modelling in static tests of space-rocket vehicles
Grebnev D.N., Duplihin V.K., Zuperman J.A., Aistov A.I., Kukushkin V.E.
Method and apparatus for evaluating the efficiency of energy transfer from combustion products to abrasive particles at the exit of a sand blaster nozzle
Kornilin D.V., Medvedev M.V.
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