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Optimization of operation mode and design parameters of a finely-dispersed metallic liquid-alloy generator
Egorychev V.S., Ryazanov A.I., Khaimovich A.I.
Optimization of model positional harakterstik of the electromagnetic sensor of the linear peremeshchny
Tingaev V.S., Matyunin S.A., Mednikov V.A.
Automation of conceptual design and modification of aircraft-type unmanned aerial vehicles using multidisciplinary optimization and evolutionary algorithms. Part 2: results and analysis
Komarov V.A., Lukyanov O.E., Hoang V., Kurkin E.I., Quijada Pioquinto J.
Automation of conceptual design and modification of aircraft type unmanned aerial vehicles using multidisciplinary optimization and evolutionary algorithms. Part 1: Methods and models
Komarov V.A., Lukyanov O.E., Hoang V.H., Kurkin E.I., QuijadaPioquinto J.G.
Optimization of the parameters of a ground speed meter of low-flying aircraft based on the application of the theory of optimal filtration
Ivanov M.E., Yezerskiy V.V.
Approximation of characteristics of linear displacement inductive sensors using modified Gaussian function with a first order difference argument
Tingaev V.S., Matyunin S.A., Mednikov V.A.
Symmetric airfoil shape optimization using the adjoint gradient method for viscous turbulent incompressible flow
Pechenik E.V.
Airfoil shape optimization using the adjoint gradient method
Pechenik E.V.
Justification of geometric parameters of the engine air particle separator
Gishvarov A.S., Rakhimov A.R.
Optimizing the process of changing spacecraft orbital parameters by using a spinning electrodynamic tether sytem
Lu H., Wang C., Zabolotnov Y.M.
Cell suspensions status monitoring by bioimpedance method
Akulov S.A., Doroshenko R.J.
The speed function of intensity of one-dimensional moving wave and it’s analysis for shock and compression waves
Arkhipova L.P.
Problems of synthesis and analysis of the system behaviour control theory on the basis of functional redundancy properties for the class of group automata
Sytnik A.A., Shulga T.E., Vagarina N.S.
Identification of a gas turbine engine mathematical model by the ressults of testing
Botchkaryov S.K., Dmitriyev A.Y.
Application of dynamic programming for path planning for observation of mobile ground targets in the controlled area
Lebedev G.N., Efimov A.V.
Model of the main worm of milling cutters for gear cutting
Androsov S.P., Brailov I.G., Vizigin D.V.
Using active noise suppression non-adaptive systems with a transfer function model for the reduction of medical equipment noise
Sementsov S.G.
Improvements in methods of analysis and control of space-rocket equipment reliability at the stage of complex electrical testing
Belova V.V.
Gas dynamic calculation of detonation in constant-cross-section ducts
Grigoriev A.V., Rudakov O.A., Solovieva A.V.
Modeling changes in a monopolist’s prices in the transition from a single price to discriminatory practices on the basis of spectral analysis
Bolochev S.A., Sitnikova A.Y.
Approximate correlative-spectral analysis of temperature patterns of combustion chambers
Prokhorov S.A., Ilinsky S.A., Aleksandrova T.G., Solovyova Y.V.
Impulse noise of digital-to-analog converters and its influence on the purity of the spectrum of digital synthesizers
Izmaylova Y.A.
Formation of light balls on the basis of interference of oncoming fine-focused beams with different polarizations
Khonina S.N., Ustinov A.
Efficiency of technical workings out in batch production GTE
Aleksentsev E.I., Shitarev I.L., Kurbatov V.P., Gritsenko E.A.
Linear mathematical model for the determination of rational treatment conditions on the finishing end milling operations in the manufacture of aircraft parts
Skuratov D.L.
Design of sheet and strip rolling modes for drawing articles with minimal earing
Grechnikov F.V., Erisov Y.A., Aryshensky E.V.
Researching error of blade locating in mechanism the POMKL–BLIK fixture by the system of approximate analysis of double-dimensional densities of probability
1 1., 1 1., 1 1., 1 1.
Determination of the maximum values of the spatial angle of attack of a nanosatellite in motion on lowcircular orbits
Glukhova L.V., Timbai I.A.
Assessment of gas turbine engine airfoil surface microstructure
Nosov N.V., Abramov A.D., Kosulin S.I.
Stabilization of steady motions of a single rotor gyrostat with a cavity filled with a liquid of high viscosity
Bezglasnyi S.P.
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.
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.
A model of monitoring the demand function in the context of a polipoly with the "ASK-RENTGEN" enterprise taken as an example
Bogatyrev V.D., Levitan V.G.
Use of approximative analysis outcome of experiment in problem of diagnostics technical conditions of hydraulic systems
Malchikov K.Y., Logvinov L.M., Kovalev M.A.
Rearrangement of digital control algorithms with variable discrete pitch size
Belonogov V.D.
Application of the artifical neyral networks theory methods for generalization and representation charachteristics of aviation gas turbine engines axial compressors
Grigoriev V.A., Kalabukhov D.S., Rad'ko V.M.
Method of fault detection and diagnosis in linear stochastic systems in the process of filtration
Tsyganova Y.V.
Choice of design characteristics of «garbage collector» spacecraft with a low-thrust electrojet engine
Ishkov S.A., Filippov G.A.
Linear mathematical model for the determination of rational treatment conditions on the diamond smoothing operations in the manufacture of aircraft parts
Skuratov D.L., Shvetsov A.N., Abulkhanov S.R.
Analysis of group properties of roller interaction in bearings using statistical
1 1.
Parametric function of differential backscattering in multiple scattered media
Zakharov V.P., Sindyaeva A.R.
1 - 41 of 41 Items

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