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Analysis of motion stability of a deployed space tether system with an atmospheric probe
Zhe D., Zabolotnov Y.M., Changqing W.
Procedure of designing a pilot operated gas pressure regulator for launch vehicle fuel tanks
Gimadiev A.G., Sverbilov V.Y., Stadnik D.M.
Dynamics of a dual-mass resonant vibration screen in a first approximation
Dentsov N.N., Koshelev A.V.
Research of repeatability of characteristics of multilayered corrugated dampers of aircraft and rocket engines using the Monte-Carlo method
Ponomaryov Y.K.
Shock wave profiles in relaxing gas with external energy source
Anchikov D.A., Galimov R.N., Zavershinskii D.I., Makaryan V.G., Molevich N.E.
Modeling thermal and thermomechanical effects in elements of microcircuits for the design of aircraft control airborne equipment
Fortinsky Y.K.
Backstepping synthesis of the height control system of an unmanned aerial vehicle
Akhramovich S.A., Barinov A.V., Malyshev V.V., Starkov A.V.
Early detection of vibration behaviour of aircraft engine multistage axial compressor in pre-surge states during rig testing
Khorikov A.A., Danilkin S.Y., Mazikina T.I.
Computation of tip clearance effect on characteristic of low pressure compressor of engine RD-33
Abdelwahid M.B., Fedorov R.M., Fedechkin K.S.
Modeling of ionization effects in integrated-circuit elements due to radiation
Fortinsky Y.K.
Сhoice of materials for producing dimensionally stable load-carrying structures
Bitkin V.E., Zhidkova O.G., Komarov V.A.
Study of characteristics of the launch vehicle fuel line gas damper
Gimadiev A.G., Odinokov D.A., Stadnik D.M., Greshnyakov P.I.
Suppression of parametric vibrations of running gear elements of tracked vehicles
Derzhanskii V.B., Taratorkin I.A., Taratorkin A.I.
Algorithms and devices for input signal identification in problems of dynamic object control and diagnostics
Zasov V.A., Tarabardin M.A., Nikonorov Y.N.
Formation of a rotating ring-shaped three-body tethered nanosatellite system with limited control
Chen S., Zabolotnov Y.M.
Frequency characteristics of a coaxial gas damper for booster feed line
Odinokov D.A., Gimadiyev A.G.
Numerical research of the static stability of honeycomb composite materials
Pershin А.M.
Method of producing thin-walled conical parts in a die with an elastic element
Popov I.P., Nesterenko E.S., Zimarev M.V.
Analysis of the influence of high-frequency current and annealing modes on the complex of mechanical properties of titanium alloy GTE compressor blades produced by high-speed stamping
Kostyshev V.A., Pityugov M.S.
Two-channel optimal discrete law of control of spacecraft with aerodynamic and inertial asymmetry during descent in Mars atmosphere
Lyubimov V.V., Bakry I.
Modeling competitive environment by the level of reliability and prices of products
Grishanova A.D., Yezhov S.Y., Tyulevina Y.S.
Stability of a rigid nonsymmetric rotor in elastic-damper sliding bearings
Ermilov Y.I.
Analysis of landing process dynamics for different reentry vehicle landing device support schemes
Borzykh S.V., Voronin V.V., Shchiblev Y.N.
Deployment and stabilization of the motion of a space tethered system in a lunar orbit
Ledkova T.A., Zabolotnov Y.M.
Analytical description of stress–strain diagram in stress and stability analysis
Saveljev L.M.
High fidelity modeling at early stages of airframe structural design
Boldyrev A.V., Komarov V.A.
Digital design of heat-resistant dimensionally stable carbon laminate (CFRP) structures
Komarov V.A., Kishov E.A., Laikova O.G., Pavlov A.A.
Mathematical model of angular motion of nanosatellites with inertial actuators
Moldabekov M.M., Ahmedov D.S., Elubaev S.A., Sukhenko A.S., Bopeev T.M., Alipbayev K.A., Mikhailenko D.L.
Stabilization of steady motions of a single rotor gyrostat with a cavity filled with a liquid of high viscosity
Bezglasnyi S.P.
Stabilization of steady motions of a single rotor gyrostat with a cavity filled with a liquid of high viscosity
Alekseev A.V., Bezglasny S.P., Krasnikov V.S.
Some questions of designing and manufacture of wire material hub dampfers
Lazutkin G.V., Parovay F.V., Troynikov A.A.
Optimal stabilization of small spacecraft angular motion in the process of deployment of an orbital tether system
Zabolotnov Y.M., Lobankov A.A.
Dynamics of spacecraft landing in the area of its contact with the surface
Voronin V.V.
3D modeling of blade flutter in modern gas turbine engines
Vedeneev V.V., Kolotnikov M.E., Makarov P.V., Firsanov V.V.
1 - 34 of 34 Items

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