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Methodology for assessing and reducing the aerodynamic imbalance of the impellers of GTE fans
Kudashov E.V., Grachev I.A., Bolotov M.A.
Development of a model for determination of preloads on blade shrouds
Pechenina E.Y., Kudashov E.V., Pechenin V.A.
Step-by-step simulation of wear of working surfaces in roller bearings
Klebanov Y.M., Murashkin V.V., Brazhnikova A.M.
Development of hydraulic devices with elastic regulating elements
Berestovitsky E.G., Gladilin Y.F., Pyalov N.V.
Development of an experimental plant and a numerical model of an axial magnetic rotor suspension
Benedyuk M.A., Lomachev A.O., Badykov R.R., Bezborodova K.V., Yurtaev A.A.
Development of microstructures for the formation of metamaterial properties of piezoelectric elements
But V.S., Kobelev A.A., Karpeev S.V.
Investigation of the edge effect in composites using the ANSYS software in a two-dimensional formulation
Skvortsov Y.V., Evtushenko M.A.
Methodological support for the training of UAV designers and operators
Lukyanov O.E., Zolotov D.V.
Forces distribution in thread and external altering load factor in thread joint under structures vibration
Kurushin M.I., Kurushin A.M., Barmanov I.S.
Computational and experimental research of exhaust gas treatment systems
Galevko V.V., Rakhmatov R.I.
Modeling of dynamic processes in micromechanical inertial sensors and their components using specialized software
Barulina M.A., Pankratov V.M.
Residual stresses distribution regularities in the smallest section of hardened hollow cylindrical detail with circular cut
Sazanov V.P., Larionova Y.S., Kolychev S.A.
Simulator, algorithm and software for the computation of differential gas circuits frequency response
Igonin A.A., Gimadiev A.G.
Method of controllung the angular position of IO ASD relative to the system of coordinates of a gyrostabilized platform
Degtyarev M.S.
Analysis of buckling of supported aircraft module skin under compressive load
1 1., 1 1.
Modeling the hypergeometric laser beam propagation using parallel computing on multi-kernel architectures
Balalayev S.A.
Determination of loads on perforated tank partition
Filipov A.G., Glazkov I.E.
Complex failure analysis of aero engine compressor blades
Sachin V.M., Tumanov N.V., Lavrentyeva M.A., Cherkasova S.A.
Development and analysis of models of heat transfer in compact porous heat exchangers of aero space control systems
Konovalov D.A.
Optimization of fatique validation cost for redesigned transport aircraft
Kleptsov V.I.
Study of residual strained state components distribution in the smallest section of superficial hardened part with a circular cut by finite-elements modeling method
Sazanov V.P.
Numerical simulation of separation processes in mechanical working
Ivanov K.M., Vinnik P.M., Ivanov V.N.
Development of a small-sized acoustic probe for the measurement of pressure pulsations in the gasdynamic duct of gas turbine engines
Gimadiyev A.G., Bystrov N.D., Ilyinsky S.A.
Mixing parameters investigations and methods of approach to calculations and development of the thrusters with a spray-centrifugal scheme of NT and NDMH mixing on the confusion chamber wall in considered
1 1.
Diffraction of the space-limited beam on the diffractive optical elements with radial symmetry
Kharitonov S.I., Kazanskiy N.L., Dmitriev A.Y.
Properties of a multi-layer multi-span corrugated package
Alkeev R.I., Suslikov V.I., Eskin I.D.
Study of mechanisms of low cycle fatigue crack propagation in aero engine disks under operating conditions and disk residual life estimation
Tumanov N.V., Cherkasova S.A., Lavrentyeva M.A., Vorobyeva N.A.
Safety front shock damper (shock absorber) to protect containers in emergency falling
Samokhin P.A., Bakhareva E.A., Potanin D.V.
Calculation of sleeve-shaped filter elements made of the MR material
Zhizhkin A.M., Lazutkin G.V., Volkova T.V.
Main results of use CAE/CAD-systems in the process of design and calculation of the working processes in internal combustion engine
Biryuk V.V., Uglanov D.A., Kayukov S.S., Gorshkalev A.A., Vakarchuk A.A., Burdanov A.M.
Method of producing thin-walled conical parts in a die with an elastic element
Popov I.P., Nesterenko E.S., Zimarev M.V.
Method of calculating vibrations in a pipeline with damping supports made of MR material
Bezborodov S.A., Ulanov A.M.
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.
Analysis of the results of fatigue tests of cylindrical specimens with fillets using the method of finite element modeling
Vakulyuk V.S.
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 schemes of correction of dynamic characteristics of acoustic probes for measuring pressure pulsations in a gas turbine engine
Gimadiev A.G., Bystrov N.D., Dyagileva E.S.
Selection of reference specimens for assessing the efficiency of part surface nitriding
Sazanov V.V.
Examination of the theoretical possibility of creating a vernier electrorocket engine
Baigaliev B.E., Chernoglazova A.V., Tumakov E.A., Temnikova S.V.
Methodology systems approach in models of technological subassembly in the aircraft industry
Barvinok V.A., Tlustenko S.F.
Finite element techniques for pipe system vibroacoustical characteristics modelling
Mironova T.B., Prokofiev A.B., Shorin V.P.
Analysis of the applicability of laser stereolithography technology for the production of turbodrives
Shabliy L.S.
Modeling stable growth of fatigue cracks in aero engine turbine discs under simple and complex loading cycles
Tumanov N.V., Lavrentyeva M.A., Cherkasova S.A., Servetnik A.N.
Forming the conceptual structure of a dimensionally stable platform by numerical optimization
Peresypkin K.V., Kozhichenkova M.S.
Control program for noncoplanar heliocentric flight to Venus of non-perfectly reflecting solar sail spacecraft
Khabibullin R.M.
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.
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.
Validation of CFD-models of gas turbine engine uncooled turbines
Matveev V.N., Popov G.M., Goryachkin E.S., Smirnova Y.D.
Development of techniques and calculation program heterogeneous gas measurement circuits
Gimadiyev A.G., Bystrov N.D., Ustinov A.
Research of the process of sheet presswork using polyurethane under constrained bending
Eskina E.V., Gromova E.G.
Construction of a blade beam finite element as a component of the blade disk rotary-symmetrical system
Davydov D.P.
Disk harmonic finite element
Davydov D.P., Ermakov A.I.
Research of dynamic parameters of hot forging on hammers with freely falling parts
Shitarev I.L., Khaimovich A.I.
Modal analysis of the dynamic mockup of “AIST–2D” small spacecraft
Igolkin A.A., Safin A.I., Filipov A.G.
Mathematical modeling of interaction a high-frequency torch discharge with construction elements of radio equipment
Kostin A.V., Piganov M.N., Stolbikov A.V.
Method of producer 3D parametric models of sample parts in SIEMNES NX
Goryachkin E.S., Rjazanov A.I., Urlapkin A.V., Chempinskiy L.A.
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.
Design procedure of factor of rigidity of aviation elastic elements
Barmanov I.S.
Formation of the light field for linear movement of a microobject
Morozov A.
Centrifugal force field effect consideration in dynamics investigation of blade wheels
Davydov D.P., Ermakov A.I.
Model of virtual balancing of rigid rotors
Khaimovich A.I., Bolotov M.A., Pechenina E.Y.
Some questions of designing and manufacture of wire material hub dampfers
Lazutkin G.V., Parovay F.V., Troynikov A.A.
Investigation of hydraulic and vibroacoustic characteristics of a prospective valve with an elastic tubular element used as the working body
Kryuchkov A.N., Romashov N.N., Ermilov M.A., Balyaba M.V.
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.
Development of magnetic fluid dampers of aicrafts chassis elements
Averianov G.S., Belkov V.N., Korchagin A.B., Agarin M.Y.
Aviation engine’s hydrodynamic bearing modeling
Parovay Y.F., Shklovets A.O.
Automated generation of structural members of a spacecraft thermal model
Kulikov D.S., Shatin A.A., Velmisov I.G.
Multi-scale complex failure analysis of aero engine compressor disks
Tumanov N.V., Porter A.M., Lavrentyeva M.A., Cherkasova S.A., Vorobyova N.A., Lyoshin D.P.
Computer simulation of thin-walled tube sink drawing
Kargin V.R., Kargin B.V., Pastushenko T.S., Yerisov Y.A.
Model for evaluating the end runouts of a rotor with parallel connections of parts
Grachev I.A., Kudashov E.V., Bolotov M.A., Pronichev N.D.
Modeling non-through surface cracks in the thin-walled structures
Skvortsov Y.V., Glushkov S.V.
Advanced methods for assessing sealing ability of valve seals
Kondrashov Y.I., Sergeev R.N.
Dynamic modelling of non-linear vibrations in cylindrical tooth gearing of aircraft drive systems
Kalinin D.V., Temis J.M.
Experimental verification of the specified characteristics of a solar battery at the stages of production and ground operation
Shuplyak Y.P., Sorokoletov V.I.
Investigation of the possibility of the creation LREST by thrust 400 N with a baffle - centrifugal scheme of NT and NDMG mixing
Ageenko Y.I., Ilin I.V., Pegin I.V., Shalamov E.A.
Analysis of stress distribution in the dangerous section area of specimens with fillets under bending using the finite-element modeling method
Vakuljuk V.S.
The influence of operational and technological factors on the dynamic parameters of elastic elements of elastic damping rotor supports
1 1., 1 1., 1 1.
Development of the finite element model of vibroacoustical characteristics of pipe system
Mironova T.B., Prokofiev A.B., Shahmatov E.V.
1 - 77 of 77 Items

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