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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.
Predicting changes in radial and axial clearances in ball bearings lubricated with low-viscosity liquids
Silayev B.M., Barmanov I.S.
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.
Gas dynamic optimization of the work process of a single-stage cooled axial turbine with an inside baffle
Popov G.M., Goryachkin E.S., Melnikov S.A., Shcherban A.I., Gataullina E.D.
Influence of complex loading of radial bearings of the oscillation groups of liquid propellant engine steering gear on the frictional moment
Balyakin V.B., Lavrin A.V., Dolgikh D.E.
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.
Application of the artifical neyral networks theory methods for generalization and representation charachteristics of aviation gas turbine engines axial compressors
Grigoriev V.A., Kalabukhov D.S., Rad'ko V.M.
Two-dimentional axial rotor compressor off-design performance prediction model with the use of simulation methods and tools
Mikhailova A.B., Akhmedzyanov D.A., Akhmetov Y.M., Mikhailov A.Y.
Computational research of multistage turbine flow taking into account flow spatial structure and associated volumes
Baturin O.V., Senchev M.N., Dzhibilov P.T.
Increasing the lifetime of power gyroscopes and momentum wheels
Khrutskaya M.V., Kamaldinov A.M.
Development of numerical models of working process in fuel auger-centrifugal pump
Gafurov S.A., Miheev M.G., Rodionov L.V., Kruchkov A.N., Shahmatov E.V.
CFD modeling of air penetration into the fuel supply pipeline
Gafurov S.A., Rodionov L.V.
About investigations the orientation dependence of single-crystal turbine blade exploitation properties
Tikhomirova E.A., Givushkin A.A., Sidokhin E.F.
Technological features of formation of the multifunctional nanostructured coverings of nitride of the titan for compressor shovels aviation GTD
Tarasenko Y.P., Tsareva I.N., Kocherov E.P., Vyazovskaya L.M.
The Laue back-reflection method for determination orientation and subgrains disorientation of blade manufacture single-crystal pieces
Tikhomirova E.A., Sidokhin 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.
The use of mathematical optimization means to increase the efficiency of a seven-stage axial flow compressor
Baturin O.V., Popov G.M., Gorachkin E.S., Novikova Y.D.
Simulation of aircraft multistage axial turbine working processes taking into account over-shroud leakage flows and blading inflows
Baturin O.V., Popov G.M., Kolmakova D.A.
Optimization of the workflow of multistage axial turbines with platforms
Matveev V.N., Baturin O.V., Popov G.M., Goryachkin E.S.
Method of calculating GTE gas-thermodynamic parameters with blade row description of an axial multistage compressor
Boyko L.G., Karpenko E.L., Akhtemenko U.F.
Formation of a method of choosing rational values of ultralow power turbine parameters in a turbine drive system
Kalabuhov D.S., Grigoryev V.A., Rad’ko V.M.
Plastic buckling of axially compressed tube
Nepershin R.I.
1 - 22 of 22 Items

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