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Title
Authors
Analysis of motion stability of a deployed space tether system with an atmospheric probe
Zhe D., Zabolotnov Y.M., Changqing W.
Dynamics of a dual-mass resonant vibration screen in a first approximation
Dentsov N.N., Koshelev A.V.
Stabilization of steady motions of a single rotor gyrostat with a cavity filled with a liquid of high viscosity
Bezglasnyi S.P.
Analysis of buckling of supported aircraft module skin under compressive load
1 1., 1 1.
Frequency characteristics of a coaxial gas damper for booster feed line
Odinokov D.A., Gimadiyev A.G.
Dynamics of spacecraft landing in the area of its contact with the surface
Voronin V.V.
Algorithms and devices for input signal identification in problems of dynamic object control and diagnostics
Zasov V.A., Tarabardin M.A., Nikonorov Y.N.
Procedure of designing a pilot operated gas pressure regulator for launch vehicle fuel tanks
Gimadiev A.G., Sverbilov V.Y., Stadnik D.M.
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.
Analysis of landing process dynamics for different reentry vehicle landing device support schemes
Borzykh S.V., Voronin V.V., Shchiblev Y.N.
Suppression of parametric vibrations of running gear elements of tracked vehicles
Derzhanskii V.B., Taratorkin I.A., Taratorkin A.I.
Optimal stabilization of small spacecraft angular motion in the process of deployment of an orbital tether system
Zabolotnov Y.M., Lobankov A.A.
Stability of a rigid nonsymmetric rotor in elastic-damper sliding bearings
Ermilov Y.I.
Formation of a rotating ring-shaped three-body tethered nanosatellite system with limited control
Chen S., Zabolotnov Y.M.
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.
High fidelity modeling at early stages of airframe structural design
Boldyrev A.V., Komarov V.A.
Deployment and stabilization of the motion of a space tethered system in a lunar orbit
Ledkova T.A., Zabolotnov Y.M.
Study of characteristics of the launch vehicle fuel line gas damper
Gimadiev A.G., Odinokov D.A., Stadnik D.M., Greshnyakov P.I.
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.
Technique for assessing the probability of survival of structural members with delaminations
Chernyakin S.A.
Analytical description of stress–strain diagram in stress and stability analysis
Saveljev L.M.
3D modeling of blade flutter in modern gas turbine engines
Vedeneev V.V., Kolotnikov M.E., Makarov P.V., Firsanov V.V.
1 - 22 of 22 Items

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