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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.
Approximation of forces of fluid film bearing lubricating layer using machine learning methods
Kazakov Y.N., Stebakov I.N., Shutin D.V., Savin L.A.
Experimental determination of damping coefficient of a support with elastic ring under harmonic loading
Diligenskiy D.S., Lezhin D.S., Novikov D.K., Luo C.
Calculation of the damping coefficient of flexible rings with working fluid
Diligensky D.S., Novikov D.K.
3D investigation of heat exchange and hydrodynamics of high pressure turbine nozzle block platforms with different cooling schemes
Gorelov Y.G., Ananyev V.V., Zolotuhina D.A.
Calculation of flow characteristics of liquid fuel supplied through pressure jet atomizers of small-sized gas turbine engines
Gurakov N.I., Zubrilin I.A., Hernandez Morales M., Yakushkin D.V., Didenko A.A., Matveev S.G., Komisar Y.V.
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.
Formation of film cooling on the turbine blade back and pressure side in the case of using V-shaped dimples
Lebedev V.V., Lebedev O.V., Remizov A.E.
Modeling of laser trimming of film resistors
Antonov J.N.
Selecting a squeeze film damper model for solving problems of gas turbine engine rotor dynamics
Leontiev M.K., Kutakov M.N.
Analysis of nonstationary thermal state of low-thrust liquid rocket engine with high-concentration hydrogen peroxide and kerosene propellant with film cooling
Vorobiev A.G., Borovik I.N., Ha S.
Mathematical models of squeeze film dampers in rotor dynamics of gas turbine engines
Kutakov M.N., Degtiarev S.A., Leontiev M.K.
Characteristics of a fuel spray downstream the pressure atomizers under high pressure in the combustion chamber
Sviridenkov A.A., Tretyakov V.V.
Build-up mathematical model of allocation temperature gas along an axis the channel a torch discharge at interaction with thick-film devices of microassambly
Stolbikov A.V., Piganov M.N., Kostin A.V.
Experimental verification of the possibility of improving the liquid propelant rocket engine performance for the “Vega” launcher upper stage
Kovalenko A.N., Pereverzev V.G., Marchan R.A., Blishun Y.V.
1 - 15 of 15 Items

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