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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.
Recurrent matrix form of the optimal elimination method
Zhdanov A.I., Yablokova L.V.
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.
Investigation of the edge effect in composites using the ANSYS software in a two-dimensional formulation
Skvortsov Y.V., Evtushenko M.A.
Solving the polynomial approximation problem with use of the iterative kachmazh method
Ivanov A.A.
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.
Applying Lagrange’s approach to solving a one-dimensional problem of wave propagation in gas in linear formulation
Nikonov V.V., Shakhov V.G.
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.
Method of orthotransformation of space images in conditions of lack of cue
Spirin A.V., Rudnev N.I., Pastuh N.K., Shuklin I.I.
Parametric function of differential backscattering in multiple scattered media
Zakharov V.P., Sindyaeva A.R.
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.
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.
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.
Structural and acoustic anisotropy of turbocompressor blade material
Tarasenko Y.P., Krivina L.A., Motova E.A., Nikitina N.Y.
Research of technological heredity influence on setting of procedure of measurements on coordinate-measurement machine in case of out-of-flatness detecting for aircraft engineering parts
Cheveleva A.O., Bolotov M.A.
Cycled pressure of the multilayered multispan packagrcorrugated package
Eskin I.D., Alkeev R.I., Ivashchenko V.I.
Lift of the airfoil with spoiler
Redkina K.V., Frolov V.A.
Methodical features of vibration tests of rotating blades using dynamic spin rigs
Nozhnitsky Y.A., Fedina Y.A., Shadrin D.V.
Application of Cebeci’s method for solving time-dependent problems of the incompressible boundary layer
Kharitonova A.N., Shakhov V.G.
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.
Three-dimensional inhomogeneous thermal fields of the “Photon-Amur 2.0” payload electronic board developed for nanosatellites
Fomin D.V., Barulinа M.A., Golikov A.V., Strukov D.O., German A.S., Ogorodnikov A.A.
Analytical determination of motion parameters of the center of mass of an uncooperative orbiter on the basis of measurement information provided by on-board systems of a space robot in a coplanar orbit
Ananenko V.M., Golyakov A.D., Kalabin P.V.
Use of the methods of the structural programming to form the «reliability» diagrams of the fuel supply system of the gas turbine engines with the control elements failure order of no less than four
Smurova N.A.
Conducting corrosion resistant nickel coating for contacts of the system of aircraft underwater locator beacons
Krivina L.A., Тsareva I.N., Tarasenko Y.P., Fel’ Y.A., Levanov Y.K.
Advanced methods for assessing sealing ability of valve seals
Kondrashov Y.I., Sergeev R.N.
Development of the method of valuating the level of competitiveness of industrial enterprises working in the sphere of space-rocket engineering
Kirilina E.V.
Comparison of focusing pulse beams with different polarization and duration by a refractive axicon
Meterko A.V., Khonina S.N.
Crystal lattice identification on the basis of assessing unit cell parameters
Kirsh D.V.
Experimental study of air flow in axisymmetric diffuser output section with rotating wall
Kurkin E.I., Ivchenko A.V.
Method of calculating vibrations in a pipeline with damping supports made of MR material
Bezborodov S.A., Ulanov A.M.
Promising technologies for solving boundary problems regarding the delivery of separating parts of carrier rockets with terminal targeting
Benevolsky S.V., Goncharenko V.I.
The results of determination angular rate and quasistatic microaccelerations the Foton S/C on the onboard measurements
1 1., 1 1., 1 1.
Calculation of durability of working section of progressive divider valve by a method of final elements
1 1., 1 1., 1 1.
Estimation the factors, make the greatest influence on reliability parametres of a GTD disk with a glance sudden failures
Belousov A.I., Gritsin A.V.
Hydrogenium saturation research for finishing pulsed electrochemical machining of titan alloy (BT9) TJ blades
Smirnov G.V.
Modeling of plant integumentary tissue influence on backscattered radiation
Bratchenco I.A., Zaharov V.P., Timchenko E.V.
Cyclic com pression of a multilayer multispan laminated package of corrugated sheets
Eskin I.D., Alkeev R.I., Ivashchenko V.I.
Assessing the strain-stress state parameters of cutting tools and parts during machining
Stepanov A.A., Haimovich A.I.
Calculation of flow characteristics of liquid fuel supplied through pressure jet atomizers of small-sized gas turbine engines
Gurakov N.I., Zubrilin I.A., Hernandez Morales M., Yakushkin D.V., Didenko A.A., Matveev S.G., Komisar Y.V.
Algorithmic method of measuring of the module of a passive complex dipole
Sharonov G.I., Shamanov R.S.
Method of design calculation jet-centrifugal gas-liquid duplex fuel nozzle with internal mixing
Egorychev V.S.
Determination of large-size liner impedance based on numerical simulation of sound propagation in a duct with specified azimuthal modal structure
Korin I.A., Palchikovskiy V.V., Pavlogradskiy V.V.
Optimization of space vehicle trans-atmospheric motion by using the method of sequential linearization
Balakin V.L., Ishkov S.A., Khramov A.A.
ASMTurbC method of autonomous statistical modeling of diffusion turbulent combustion and the results of its testing
Nuzhnov Y.V.
Parameters transducers of the blade’s dynamic movements of turbounits based on nonlinear approximation of primary signals
Chernyavskiy A.Z., Danilin A.I., Danilin S.A.
Modelling the propagation of sharp focused laser beams through scanning probes of different shapes
Degtyaryov S.A., Khonina S.N., Skuratov D.L.
Nonparaxial iterative calculation of diffractive optical elements focusing in a subwave light spot
Bogdanova E.Y., Khonina S.N.
Trouble error parameters determination microrelief optoelectronic means on the basis of correlation algorithm
Abramov A.D., Bukanov F.F.
Design of robust systems for the stabilization of unmanned aircraft equipment
Sushchenko O.A., Azarskov V.N.
Technique of operational monitoring of blade operational life exhaustion on turbounits
Danilin A.I., Grechishnikov V.M.
Obtaining the analytical solution of the heat boundary layer equation based on introducing additional boundary conditions
1 1., 1 1.
The flowing reactor as the tool of an experimental research of processes of transformation self-igniting liquid rocket fuel
1 1., 1 1.
Processing of experimental data by the method of the least squares
Ovchinnikov A.V., Krasnochub E.K., Bronstein V.M.
Multi-time-step scheme in the vorticity splitting method applied to the simulation of the wake behind the flat plate
Nikonov V.V., Shakhov V.G.
Propagation of laser vortex beams with an arbitrary topological charge in a craded-index parabolic fiber
Strilets A.S.
Verification of a complex of mathematical models of aerodynamics and dynamics of Savonius rotor motion
Sizov D.A., Onushkin Y.P., Krasnova O.A., Dzhanibekov O.T.
Forming the conceptual structure of a dimensionally stable platform by numerical optimization
Peresypkin K.V., Kozhichenkova M.S.
Influence of deviations in manufacturing of electrothermal propulsion system on nanosatellite maneuvering accuracy
Sinitsin L.I., Belokonov I.V.
Research of dynamic parameters of hot forging on hammers with freely falling parts
Shitarev I.L., Khaimovich A.I.
Modeling of redistribution of residual stresses in the cylindrical specimens after advancing surface plastic forming
Chirkov A.V., Sazanov V.P., Samoylov V.A., Larionova Y.S.
Optimization of space vehicle combined orbital plane change maneuver on the basis of the successive linearization method
Balakin V.L., Ishkov S.A., Khramov A.A.
Safety front shock damper (shock absorber) to protect containers in emergency falling
Samokhin P.A., Bakhareva E.A., Potanin D.V.
Multichannel blind image deconvolution algorithm
Berezowskii A.A., Goryachkin O.V.
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