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Verification of aero-engine numerical rotor models based on virtual static structural and modal tests
Shaposhnikov K.V., Degtyarev S.A., Leontiev M.K., Anisimov S.V.
Ensuring vibration characteristics of reactor plant centrifugal pumping equipment
Savchuk D.V., Bescherov D.E., Kulikov D.A., Panov V.A., Patrushev V.L., Porfiriev M.S., Soloviev S.A.
Verification of a transonic stage CFD model for assessing the erosion wear influence on the operation of the axial compressor
Blinov V.L., Zubkov I.S.
Comparative analysis of turbulence model influence in numerical simulation of an experimental radial compressor stage
Eremenko V.V., Mikhailov A.E., Mikhailova A.B., Goryukhin M.O., Krasnoperov D.G.
Research of rotor dynamic of GTE with nonlinear stiffness of elastic elements in support parts
Leontyev M.K., Tereshko A.G.
Application of open-source software for industrial problems of vehicle lift-off gas dynamics
Abdurashidov T.O., Osipov A.V., Korchagova V.N., Kraposhin M.V., Smirnova Y.V., Strizhak S.V.
Method of calculating dynamic designs of space launch vehicles for designing systems of stabilization of their motion
Lobanov V.A.
Mathematical models of squeeze film dampers in rotor dynamics of gas turbine engines
Kutakov M.N., Degtiarev S.A., Leontiev M.K.
Characteristic of energy efficiency index and drawing intermediate conclusions on the reduction of consumption of energy resources at SSAU
Anishchenkova E.I., Biryuk V.V., Anisimov M.Y.
Key focus areas of samara state aerospace university research and education center of gasdynamic research
Matveev V.N., Anisimov M.Y.
The calculated study of fluid structure in a hub an axial aviation turbine
1 1., 1 1.
Сalculated analysis of the influence of operation and design factors on the parameters of oxygen-hydrogen low-thrust rocket engines
Ryzhkov V.V., Morozov I.I.
Van der Pol, Rayleigh and Duffing oscillators in discrete time dynamics
Zaitsev V.V., Nuraev D.B., Shilin A.N.
Research of a sleeve connection of the aircraft pipeline under the influence of dynamic loading
Agafonov V.M., Pykhalov A.A.
Numerical modeling on dynamic process of injection in supersonic part of the nozzle
Yakovchuk M.S.
Optimization characteristics of rotor-support system from NK-14ST free power turbine with consider statics and dynamics propertys
1 1., 1 1.
Dynamics of a dual-mass resonant vibration screen in a first approximation
Dentsov N.N., Koshelev A.V.
Perfecting the methodology of determining the flexibility matrix of the «squirrel cage» in rotor supports of aviation gas-turbine engines
Degtyarev S.A., Leontiev M.K., Popov V.V.
Research of small spacecraft dynamiсs taking into account the influence of elastic vibrations of asjacent solar panels and aerodynamic moment
Yelenev V.D., Titov B.A., Davydov E.I., Davydov I.E., Kochyan A.G., Yudintsev V.V.
Uniform and equidistant ways of structured computation grigd creation for CFD problems
Yefimow A.N., Matveev V.N.
Formation of a rotating ring-shaped three-body tethered nanosatellite system with limited control
Chen S., Zabolotnov Y.M.
Schemes, parameters, work process, characteristics and structure of long-range interception aircraft engines
Kovalev A.V., Sanin V.N., Krivenok A.G., Korolenko V.V.
System-mathematical simulation of engine air hydraulic power supply
Goryunova N.R., Goryunov A.A.
Investigation of 11D428А-22 thruster operation dynamics with bellows flow stabilizer
Beshenev Y.A., Volkov A.V., Kazankin F.A.
Rotor in gas bearings dynamics experiment-calculated investigation
Temis Y.M., Temis M.Y., Egorov A.M., Gavrilov V.V., Ogorodov V.N.
Mathematical model of sequential feeders for centralized lubrication systems
Rybaltchenko D.Y., Shakhmatov Y.V., Belov G.O., Ilyukhin V.N.
Gas-dynamic losses in the flow part of the channel charge of a solid-propellant rocket engine
A. N. Sabirzyanov A.N., Khamatnurova C.B., Kuzmin V.V.
Service-oriented distributed software complex for evaluation and multi-criteria analysis of reliability and survivability of on-board equipment of small satellites: Russian and Belarusian segments
Zelentsov V.A., Potryasaev S.A., Sokolov B.V., Skobtsov V.Y., Korenyako S.A., Kim D.S., Vakulchyk E.N., Kulbak L.I., Nikolaenya E.D., Lapitskaya N.V., Saksonov R.V.
Experimental research of combined technology for parts assembly
Glushchenkov V.A., Khardin M.V., Belyaeva I.A.
Peculiarities of modeling the work process in a low-pressure compressor of a gas turbine plant
Matveev V.N., Popov G.M., Goryachkin E.S., Smirnova Y.D.
Experimental investigation of turbulence of influence of the compressor’s out flow parameters on the hydraulics parameters resistance of separation diffuser of combustion chamber
Guryanova M.M.
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.
Gasdynamic and strength improvement of the axial flow turbine of a helicopter gas turbine engine
Goriachkin E.S., Popov G.M., Matveev V.N., Shcherban A.I., Kudryashov I.A., Melnikov S.A.
Mathematical simulation of combined technologies
Belyaeva I.A.
“Squirrel cage” flexibility in supports of aviation gas turbine engine rotors
Degtiarev S.A., Leontiev M.K., Popov V.V.
Kinematic and dynamic analysis of the basic mechanism of the Wankel engine, based on its vector model
Kosenok B.B.
CFD-based modeling of oil ang gas journal bearings using commercial software packages
Pugachev A.O., Ravikovich Y.A., Ermilov Y.I., Kholobtsev D.P., Matushkin A.A.
Special aspects of numerical simulation of a two-stage axial-flow compressor with defective blades
Blinov V.L., Zubkov I.S., Iskortsev E.Y., Belyaev O.V., Plishkin P.I.
Application of decision support technology at various stages of the life cycle of space facilities in assembly with the information system of technical condition and reliability
Avtamonov P.N., Bakhmut A.D., Krylov A.V., Okhtilev M.Y., Okhtilev P.A., Sokolov B.V.
CIAM’s scientific school of strength and its ties with Samara aerospace cluster (for the 85 th anniversary of CIAM’s foundation)
Nozhnitskiy Y.A., Belousov A.I., Kotcherov E.P.
Problems and solutions of using computer technologies in designing of combustion chambers GTE
Matveev S.G., Orlov M.Y., Zubrilin I.A.
Dynamic analysis and optimization of turbojet engine nozzle control mechanism
Parametrical design of discrete mapping of Van der Pol oscillator
Zaitsev V.V., Nuraev D.B., Yudin A.N.
System of differential equations of aircraft spatial motion dynamics with arbitrary tensor of inertia and center of gravity position
Vereshchikov D.V.
Application of Bubnov-Galerkin method to determine fixed vibrational loads of launch vehicle compartments
Popov P.A., Sindyukov A.A., Malykhina O.I.
Strength analysis of internal combustion engine elements by using ANSYS with taking into account heat processes in the combustion chamber
Biryuk V.V., Gorshkalev A.A., Kayukov S.S., Saigakov E.A.
Dynamics of spacecraft landing in the area of its contact with the surface
Voronin V.V.
Mathematical model of complex spatial deformation of rotor blades during helicopter arbitrary motion
Girfanov A.M.
Analysis of landing process dynamics for different reentry vehicle landing device support schemes
Borzykh S.V., Voronin V.V., Shchiblev Y.N.
1 - 49 of 49 Items

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