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Comparison of quasi-three-dimensional and full three-dimensional formulations of thrust bearing operation
Sokolov N.V., Khadiev M.B., Fedotov P.E., Fedotov E.M.
Analysis of ablation process method errors for the definition of the temperature profile of high-temperature gas flows
Shustov S.A.
New technologies of manufacturing non-rigid parts made of titanium alloys and stainless steels
Kiselev E.S., Blagovskiy O.V.
Influence of the strengthening-finishing treatment on structure-energy state of surface layer and fatigue resistance
Sazonov M.B., Volkov A.N., Schigrinyev I.A.
Stability of a rigid nonsymmetric rotor in elastic-damper sliding bearings
Ermilov Y.I.
Numerical model of viscosity impact on flow in low-thrust rocket engine nozzles in the approximation of a laminar boundary layer with velocity slip
Shustov S.A.
Mathematical model of surface layer formation during hydroabrasive jet machining
Meshcheryakov A.V., Shulepov A.P.
Reduction of friction on a flat plate in the presence of a fluid film on its surface
Klyuev N.I., Frolov V.A., Kryukov Y.A.
Gas-discharge generation of near-wall flows
Ivchenko A.V., Zhuravliov O.A., Shakhov V.G.
Improvement of adhesive properties and load capacity of the lubricant layer of friction units
Gromakovsky D.G., Koptev A.A., Kryshen E.D., Haustov V.I., Shigin S.B.
The dependence of detail fatigue resistance on the thickness of hardening layer under outstripping superficial plastic deforming
Vakuljuk V.S.
Problems and prospect of microgasturbines development for unmanned aerial vehicle propulsion
Zhdanov I.A., Staudacher S., Falaleev S.V.
Experimental research of wall boundary flow formation in the combustion chamber of a small gas generator with self-igniting fuel components
Shustov S.A.
Application of the technology of pulsed laser surface coating in correcting casting defects of parts made of «ЖС-32» alloy
Smelov V.G., Sotov A.V., Agapovichev A.V., Nosova E.A.
Aviation engine’s hydrodynamic bearing modeling
Parovay Y.F., Shklovets A.O.
Numerical investigation of gas dynamics in nozzles of small-dimensioned gas generators and flowing out jets
Ivanov I., Kryukov I., Shustov S.
Improvement of the quality of the surfaces of monowheel blades of liquid rocket engine turbopump assemblies
Mozgov S.A., Panov D.V., Saushkin B.P.
Primary assessment of the effects of temperature drop on the mechanical properties of a protective oxide layer obtained by microarc oxidation on alloy AK9
Krishtal M.M., Ivashin P.V., Pavlov D.A., Polunin A.V.
Interaction of exhaust jets of rocker propulsions on various propellants with atmosphere for estimation of ecological safety of firing of rockets and launchers
Zavelevich F.S., Ushakov N.N.
Application of Cebeci’s method for solving time-dependent problems of the incompressible boundary layer
Kharitonova A.N., Shakhov V.G.
Experimental research of the possibility of heat transfer enhancement in gas dynamic energy separation process
Popovich S.S., Vinogradov Y.A., Strongin M.M.
Formation of the sliding surface mechanical seal different methods
Tarelnik V.B., Martsinkovskiy V.S., Antoshevskiy B.
Obtaining the analytical solution of the heat boundary layer equation based on introducing additional boundary conditions
1 1., 1 1.
Definition of the apparent elastic limit's change in metal materials at nanoporous structures formation
Murzin S.P., Tregub V.I., Osetrov E.L.
Development of the technology of diagnostics of turbo-jet aviation engines by a filtering element with a diagnostic layer
Drokov V.V., Drokov V.G., Muryshenko V.V., Mukhutdinov F.I., Khaliullin V.F.
Research of influence of methods SPD on stpucture surface layer and resistance of fatigue
Volkov A.N., Sazonov M.B., Schigrinyev I.A.
The determination of the efficient parameters of surface strenghtening the thin-walled and the small-hard parts of gas turbine engines based on deformation tolerance
1 1., 1 1.
Calculation of lubricant flow in the slide bearing of the aviation engine reducer
Siluyanova M.V., Fertikov A.О.
Designing of low-flow rate slider bearings for turbomachinery rotors
Parovay E.F.
Influence of the direction of ultrasonic vibrations on the formation of residual stresses in thread pieces made of titanium alloys
Romashkina O.V., Karanaeva O.V.
Experimental analysis of flow separation in low thrust rocket engine nozzles with a profiled supersonic part of the nozzle
Shustov S.A.
1 - 31 of 31 Items

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