About the probes for measuring pulsations of pressure in the flowing part gas turbine engines
Shorin V.P., Gimadiev A.G., Bystrov N.D., Ilinskij S.A.
Structure of arterial blood pressure monitors
Fedotov A.A., Akulov S.A., Akulova A.S.
The analysis of real thermodynamic cycle of bypass engine with mixing
Medvedev V.V.
Pilot study of frequency characteristics of an acoustic probe for measuring pressure pulsations in the gas turbine engine inlet device
Ivanenko V.N., Alexandrova T.G., Dyagileva E.C., Gimadiyev A.G., Bystrov N.D.
Modeling static and dynamic characteristics of pressure reducing valves
Igolkin A.A.
Numerical simulation of tonal noise of a bypass engine fan stage
Pyatunin K.R., Arharova N.V., Remizov A.E.
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.
Development of methods of modeling and computer-aided design of compressors
Krivosheev I.A., Rozhkov K.E.
Ways of improving burners of two-staged combustion chambers
Bantikov D.Y., Grechishnikov O.V., Rogalev V.V., Roslyakov A.D., Tsybizov Y.I.
Constructive actions for decreasing the acoustic pressure inside space-rocket products
Popov P.A., Sindyukov A.A.
Method of reducing design aerodynamic characteristics to the results of drain tests of a transport category aircraft model
Bondar Y.I.
Design and research of characteristics of a pressure fluctuation damping device for electrocontact manometers
Gimadiev A.G., Gimadiev A.A., Ermochkin A.Z., Ilyuchin V.N.
Modeling thermal and thermomechanical effects in elements of microcircuits for the design of aircraft control airborne equipment
Fortinsky Y.K.
Analysis of the effect of technological parameters of rolling on the optimization of rolling milladjustment programs
Tlustenko S.F.
Wearability, wearproof and heat-shielding coverings for details of the gas path of the turbine, the compressor and the chamber of combustion of gas turbine engine
Barvinok V.A., Shitarev I.L., Bogdanovich V.I., Dokukina I.A., Karasev V.M.
Influence of tension and contact stress on sliding in cylindrical roller bearings in support of gas turbine engines
Belomytcev O.M., Pischalnikov A.B.
Characteristics of the sampling instrument for measuring emissions of an aircraft gas turbine engine
Okhlobystin A.V., Lyubimov R.V., Sokolova N.N.
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.
Calculation of hydrodynamic noise in the diffuser of a pulsation damper flow channel
Makaryants G.M., Gafurov S.A., Zubrilin I.A., Kryuchkov A.N., Shakhmatov Y.V., Berestovitsky E.G., Gladilin Y.A.
Calculating sound insulation of a sandwich structure on the basis of the «inverse matrix» method
Popov P.A., Osipov A.S., Sindyukov A.A.
Elimination of gas dynamic resonance modes of vibration loads of gas distribution station pipeline fitting
Shabanov K.U., Kryuchkov A.N., Ermilov M.A., Balyaba M.V.
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.
Physical principles of hydrodynamic non-stationarity effect on turbulent flow
Krayev V.M., Tikhonov A.I.
Simulating of Roots compressor
Belov G.O., Ermilov M.A., Kryuchkov A.N.
Elastic metal-plastic thrust bearings for combined hydraulic units of pumped storage hydroelectric power stations
Baiborodov Y.I.
Pressure pulsation dampener for air controller
Igolkin A.A., Safin A.I., Shakhmatov E.V.
Increasing efficiency of pressurization of the rocket tanks in the flight
Biryuk V.V., Kapitonov V.A., Smorodin A.V.
Design of bimetallic impeller for gas turbine
Magerramova L.A.
Analysis of schemes of correction of dynamic characteristics of acoustic probes for measuring pressure pulsations in a gas turbine engine
Gimadiev A.G., Bystrov N.D., Dyagileva E.S.
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.
Choosing the aerodynamic configuration of a subsonic cruise missile
Kovalev M.A., Nikitin A.N.
On the development of probes for measuring pressure pulsations in the gas-dynamic channel gas generator
Shorin V.P., Gimadiyev A.G., Bystrov N.D., Ilyinsky S.A., Alexandrova T.G.
Dynamic tests of probes for measurement of pulsations pressure at the raised average pressure
1 1., 1 1., 1 1., 1 1.
Development of a small-sized acoustic probe for the measurement of pressure pulsations in the gasdynamic duct of gas turbine engines
Gimadiyev A.G., Bystrov N.D., Ilyinsky S.A.
Vortex cleaning of fuel tank pressurant gas
Biryuk V.V., Shimanov A.A., Onoprienko D.A., Smorodin A.V., Shepelev A.I.
Measurements of pulse pressures within the volume of a melt in terms of intense impulse interferences
Yusupov R.Y., Kostryukov E.E.
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.
Dependence of energy characteristics of Stirling gas refrigerating machines on external and internal parametric values
Belozertsev V.N.
Pressure measurements in the pipelines with the help of combined high temperature pressure sensor
Limanova N.I., Yudin P.E., Limanov I.A.
Dynamic of the a safety vent valve
Makaryjants M.V., Kudyurov L.V., Mustafaev Y.K., Tumanov D.V.
Stabilization of a pilot-operated gas pressure control valve by placing a throttle at the inlet
Stadnik D.M., Sverbilov V.Y., Makaryants G.M., Makaryants M.V.
Theoretical definition of temperature fields at thermoplastic hardening of details of gas turbine engines
Barvinok V.A., Vishnyakov M.A., Ignatiev S.A.
Fluctuations of pressure in rail gas injection of engines with spark ignition
Shishkov V.A.
Calculation of lubricant flow in the slide bearing of the aviation engine reducer
Siluyanova M.V., Fertikov A.О.
Life testing of pipeline elements
Boltenkova O.M., Davydov O.Y., Yegorov V.G.
Theoretical and experimental studies of a gas stamping device with a piston pressure multiplier
Botashev A.Y., Bayramukov R.A.
Assessment of changes in the sound-proof ability of the rocket fairing with layers of sound-proof materials varying in thickness
Popov P.A.
The equipment for research of properties of hydrocarbons at pressure from above 150 MPа
Rednikov S.N.
Calculated study of tangential inclination of nozzle vanes influence on gas-dynamic efficiency of axial turbine stage
Baturin O.V., Matveev V.N.
Impact of the turbulence modeling approach on the accuracy of the fan noise level prediction
Pyatunin K.R., Arkharova N.V.
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.
Computation of tip clearance effect on characteristic of low pressure compressor of engine RD-33
Abdelwahid M.B., Fedorov R.M., Fedechkin K.S.
Development and research of a device for gas sheet stamping with a piston pressure multiplier
Botashev A.Y., Bayramukov R.A.
The influence of a combined pump’s auger-centrifugal stage inlet design on its vibration and pulsation states
Gafurov S.A., Rodionov L.V., Kryuchkov A.N., Makaryants G.M., Shakhmatov Y.V.
Analysis of control programs and climb paths of the hypersonic first stage of an aerospace system
Balakin V.L., Krikunov M.M.
Biological module “BiNOM” for cubesats of the SamSat family
Zakharov V.P., Konyukhov V.N., Bakhtinov P.I., Molchkov E.V., Kornilin D.V., Konovalov S.G.
Switched-reactance control of pressure and flow as a way to increase energy efficiency of hydraulic drives – a state-of the-art review
Sverbilov V.Y., Stadnik D.M., Iliukhin V.N., Shamin D.V.
Pressure pulsation dampers as a means of improving the inherent vibroacoustic charateristics of hydraulic test rigs
Berestovitsky E.G., Gladilin Y.A., Kryuchkov A.N., Fyodorov A.Y., Frantov A.A., Shakhmatov Y.V.
Relation between flame chemiionization and variable-volume combustion chamber temperature and pressure
Shaikin A.P., Galiev I.R.
Development of discrete pneumatic pressure regulator and researching of its characteristics
Greshniakov P.I., Sinyakov A.F., Ilukhin V.N.
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.
Comparison of mathematical simulation results and experimental research of PVD-K3-1 air pressure probe
Moiseev V.N., Dubinina M.M., Pavlovsky A.A., Sorokin M.Y.
Flow conditioning downstream a pressure collector
Kalaev V.A., Khorobrov S.V.
Choosing the optimal method of the centrifugal loads modeling using 2D FE models of the compressor’s disks slots
Balyaeva N.N., Guschin A.Y.
Analysis of contact stresses in drawing round products
Kargin V.R., Kargin B.V., Kolesnikova S.Y., Sergeev Y.A.
Designing of the aviation engine's hydrodynamic bearing
Parovay Y.F., Gordeev V.B., Falaleev S.V.
Characteristics of a fuel spray downstream the pressure atomizers under high pressure in the combustion chamber
Sviridenkov A.A., Tretyakov V.V.
Cycled pressure of the multilayered multispan packagrcorrugated package
Eskin I.D., Alkeev R.I., Ivashchenko V.I.
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.
Development of a pulsation dampener for hydraulic systems of power plants
Kryuchkov A.N., Еrmilov M.A., Еrmilova E.N., Balakhonov I.V., Vidyaskina A.N.
Mathematical model of investigating normal acoustic modes of launch vehicle modules
Popov P.A., Belov A.S., Kryuchkov A.N.
Procedure of designing a pilot operated gas pressure regulator for launch vehicle fuel tanks
Gimadiev A.G., Sverbilov V.Y., Stadnik D.M.
Influence of the loading parameter on the efficiency ofa three-stage turbine of turbojet bypass engine
1 1., 1 1.
The fiber-optical multitouch pressure transducer
Leonovich G.I., Matjunin S.A., Livochkina N.A.
Review of research conductivity of dielectrics and semiconductors under high pressure
Telegin A.M., Kalaev M.P., Semkin N.D.
Fiber-optical pressure transducer for the UA engine control system
Leonovich G.I., Matyunin S.A., Glushkov A.I., Livochkina N.A., Solovyov V.I.
Research of current and power interchange of swirled fluid streams in a hydraulic heat gentrator
Belozertsev V.N.
Research of the wet condition in fuel tanks of high weight booster rockets during storage and aviation transportation periods
1 1., 1 1., 1 1.
Experimental research of staff LTRE with hypergolic propellant under impulse engaging conditions
Shustov S.A.
Dependence between microscopic characteristics of the material MR and parameters of press forming
1 1., 1 1.
Test bench for investigation of thrusters intra-chamber working processes
Pervyshin A.N., Ryazanov A.I.
Shaping parts explosive processes on conditions exactly assembly aircraft components
Tlustenko S.F., Sitnik V.A.
Application of Bubnov-Galerkin method to determine fixed vibrational loads of launch vehicle compartments
Popov P.A., Sindyukov A.A., Malykhina O.I.
Increasing efficiency of pressurization of the rocket tanks in the flight
1 1., 1 1.
To a question of forcing up of thermal stirlings macine
Belozertcev V.N.
The efficiency of aligning gratings at engine inlet of ground power plants
1 - 86 of 86 Items

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