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Authors
Analysis of information characteristics of a dynamic displacement doppler transducer signal
Danilin A.I., Gretskov A.A.
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.
Research of possibilities to obtain high-alloy aluminummagnesium alloys
Grechnikov F.V., Popov I.P., Bibikov A.M., Demyanenko E.G.
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.
Methods of protecting unpressurized compartments of spacecraft from the penetration of electromagnetic field
Syomkin N.D., Balakin V.L., Bragin V.V.
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.
Analytical approximation of aircraft dynamics model in problems of approximate optimal control synthesis
Blinov A.O., Gurman V.I., Fralenko V.P.
Method of calculating of the load characteristics of cylindrical support with a discrete location of elastic damping elements of the MR material
1 1., 1 1., 1 1., 1 1., 1 1.
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.
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.
Experimental research of wall boundary flow formation in the combustion chamber of a small gas generator with self-igniting fuel components
Shustov S.A.
Influence of deviations in manufacturing of electrothermal propulsion system on nanosatellite maneuvering accuracy
Sinitsin L.I., Belokonov I.V.
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.
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 climb paths of the hypersonic first stage of an aerospace system
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.
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.
Design procedure of factor of rigidity of aviation elastic elements
Barmanov I.S.
Methods and the experiment of the parametric identification compressors and fans mathematical models of according to the results of the gas turbine engine development test
Kofman V.M.
Optimum programs of correction of quasielliptical and circular orbits of spacecraft with the limited-thrust engine
Khramov A.A.
Research and rationing admissible nick on working blades of the compressor for engine NK-12 example
1 1., 1 1., 1 1., 1 1.
Decrease in toxicity of transport diesel engines by neutralisation nitrogen oxide of the fulfilled gases
1 q., 1 1.
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.
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 calculating self-capacitance in planar structural elements of a spacecraft
Syomkin N.D., Bragin V.V., Pomelnikov R.A., Balakin V.L.
Disturbed transatmospheric motion of the first stage of an aerospace system
Krikunov M.M.
Algorithmic method of measuring of the module of a passive complex dipole
Sharonov G.I., Shamanov R.S.
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.
Numerical simulation of low liquid flow in a mixer consisting of two centrifugal swirlers
Semkin E.V.
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.
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.
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.
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.
Application of Cebeci’s method for solving time-dependent problems of the incompressible boundary layer
Kharitonova A.N., Shakhov V.G.
The results of determination angular rate and quasistatic microaccelerations the Foton S/C on the onboard measurements
1 1., 1 1., 1 1.
Improving the operating characteristics of engines by the imposition of manufacturing operation of hermeticity inspection of vacuum-tight radio electronic device cases
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.
The devices for the diagnosis and control of turbine blades deformative condition during operation
Danilin A.I., Chernyavskiy A.G., Kapustin A.S.
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.
Limit values of the Brayton cycle with the use of reduced fuel characteristics
Mikheenkov E.L., Nekrasova S.O.
Properties of a multi-layer multi-span corrugated package
Alkeev R.I., Suslikov V.I., Eskin I.D.
Method and technical tools of assessing the reliability of digital angle converters
Grechishnikov V.M., Yudin A.A.
Method of design calculation jet-centrifugal gas-liquid duplex fuel nozzle with internal mixing
Egorychev V.S.
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.
Development of the method of valuating the level of competitiveness of industrial enterprises working in the sphere of space-rocket engineering
Kirilina E.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.
Comparison of focusing pulse beams with different polarization and duration by a refractive axicon
Meterko A.V., Khonina S.N.
EDM laser alloying and texturing the sliding surface mechanical seals
Antoshevskiy B., Tarelnik V.B., Martsinkovskiy V.S.
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.
Obtaining the analytical solution of the heat boundary layer equation based on introducing additional boundary conditions
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.
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.
Ensuring efficient operation of roller bearings
Grechishnikov O.V., Balakin A.Y., Roslyakov A.D.
101 - 169 of 169 Items << < 1 2 

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