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Constructive actions for decreasing the acoustic pressure inside space-rocket products
Popov P.A., Sindyukov A.A.
Simulating of Roots compressor
Belov G.O., Ermilov M.A., Kryuchkov A.N.
Step-by-step simulation of wear of working surfaces in roller bearings
Klebanov Y.M., Murashkin V.V., Brazhnikova A.M.
Analysis of the influence of lubricant supply conditions on the pressure distribution in squeeze-film dampers
Novikov D.K., Shliandina N.S.
Developing an electronic reference book on thermogasodynamic properties of rocket engine fuel combustion products taking into account non-ideal character of the working process
Silyutin M.V.
Test bench for investigation of thrusters intra-chamber working processes
Pervyshin A.N., Ryazanov A.I.
Research of current and power interchange of swirled fluid streams in a hydraulic heat gentrator
Belozertsev V.N.
Life testing of pipeline elements
Boltenkova O.M., Davydov O.Y., Yegorov V.G.
Calculated study of tangential inclination of nozzle vanes influence on gas-dynamic efficiency of axial turbine stage
Baturin O.V., Matveev V.N.
To a question of forcing up of thermal stirlings macine
Belozertcev V.N.
Vortex cleaning of fuel tank pressurant gas
Biryuk V.V., Shimanov A.A., Onoprienko D.A., Smorodin A.V., Shepelev A.I.
Assessment of changes in the sound-proof ability of the rocket fairing with layers of sound-proof materials varying in thickness
Popov P.A.
Method of reducing design aerodynamic characteristics to the results of drain tests of a transport category aircraft model
Bondar Y.I.
Increasing efficiency of pressurization of the rocket tanks in the flight
Biryuk V.V., Kapitonov V.A., Smorodin A.V.
Calculation of lubricant flow in the slide bearing of the aviation engine reducer
Siluyanova M.V., Fertikov A.О.
Estimation of static strength of sections of the linear pipeline portion with a colony of corrosion fine cracks
Subbotin V.A., Scherbo I.V., Kholodkov S.A., Giorbelidze M.G.
Analysis of the effect of technological parameters of rolling on the optimization of rolling milladjustment programs
Tlustenko S.F.
Peculiarities of acoustic loading of the space vehicle in the nose fairing launched as part of a «Soyuz»-type rocket
Popov P.A., Sindyukov A.A., Kryuchkov A.N.
Impact of the turbulence modeling approach on the accuracy of the fan noise level prediction
Pyatunin K.R., Arkharova N.V.
Dependence of energy characteristics of Stirling gas refrigerating machines on external and internal parametric values
Belozertsev V.N.
The equipment for research of properties of hydrocarbons at pressure from above 150 MPа
Rednikov S.N.
Elastic metal-plastic thrust bearings for combined hydraulic units of pumped storage hydroelectric power stations
Baiborodov Y.I.
System of pressurization of the fuel tank of a launch vehicle using the heat of generator gas
Biryuk V.V., Smorodin A.V., Shepelev A.I., Onoprienko D.A.
Relation between flame chemiionization and variable-volume combustion chamber temperature and pressure
Shaikin A.P., Galiev I.R.
Dynamic of the a safety vent valve
Makaryjants M.V., Kudyurov L.V., Mustafaev Y.K., Tumanov D.V.
Calculating sound insulation of a sandwich structure on the basis of the «inverse matrix» method
Popov P.A., Osipov A.S., Sindyukov A.A.
Full-scale tests of superloaded thrust bearings for hydraulicturbine generators of Sibir hydroelectric power stations of the new generation with unit power of 1 million kw
Baiborodov Y.I.
Application of Bubnov-Galerkin method to determine fixed vibrational loads of launch vehicle compartments
Popov P.A., Sindyukov A.A., Malykhina O.I.
Numerical simulation of tonal noise of a bypass engine fan stage
Pyatunin K.R., Arharova N.V., Remizov A.E.
Analysis of contact stresses in drawing round products
Kargin V.R., Kargin B.V., Kolesnikova S.Y., Sergeev Y.A.
Dependence between microscopic characteristics of the material MR and parameters of press forming
1 1., 1 1.
Characteristics of a fuel spray downstream the pressure atomizers under high pressure in the combustion chamber
Sviridenkov A.A., Tretyakov V.V.
Shaping parts explosive processes on conditions exactly assembly aircraft components
Tlustenko S.F., Sitnik V.A.
Cramped bending of sheet metal piece curved sides with an elastic medium
Barvinok V.A., Komarov A.D., Kulakov V.G., Moisseyev V.K., Sharov A.A.
Increasing efficiency of pressurization of the rocket tanks in the flight
1 1., 1 1.
Review of research conductivity of dielectrics and semiconductors under high pressure
Telegin A.M., Kalaev M.P., Semkin N.D.
Mathematical model of investigating normal acoustic modes of launch vehicle modules
Popov P.A., Belov A.S., Kryuchkov A.N.
Structure of arterial blood pressure monitors
Fedotov A.A., Akulov S.A., Akulova A.S.
1 - 38 of 38 Items

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