Influence of energy separation and vortex tube geometry on the flow turbulence
Piralishvili S.A.
Device for rejection of semiconductor diodes
Tyulevin S.V., Piganov M.N., Chopin G.P., Arhipov A.I.
Efficiency of complex cycles of a gas turbine unit with varying degrees of heating in the first and second stages
Ivanov V.A.
Development of methods of designing modern gas turbines
Inozemtsev A.A., Khairulin V.T., Tikhonov A.S., Samokhvalov N.Y.
Analysis of the thermal state of aircraft engine supports
Vinogradov A.S., Badykov R.R., Fedorchenko D.G.
Limit values of the Brayton cycle with the use of reduced fuel characteristics
Mikheenkov E.L., Nekrasova S.O.
Choice of materials for making inductor systems
Barvinok V.A., Palamartchuk Y.Y., Kirilin A.N., Samokhvalov V.P., Vershigorov V.M.
Optimization of the workflow of multistage axial turbines with platforms
Matveev V.N., Baturin O.V., Popov G.M., Goryachkin E.S.
Modelling of an ejector for turbine aeroengines for application in performance synthesis tools
Georgi J., Staudacher S., Falaleev S.V.
Mathematical modeling of dynamic processes in a hydraulic drive with a discrete regulator of liquid flow
Shakhmatov Y.V., Gimadiev A.G., Sverbilov V.Y., Sinyakov A.F.
Characteristic of energy efficiency index and drawing intermediate conclusions on the reduction of consumption of energy resources at SSAU
Anishchenkova E.I., Biryuk V.V., Anisimov M.Y.
Rail electromagnetic accelerators with an external magnetic field
Sukhachev K.I.
Ways to improve the workflow of liquid rocket thrusters on hypergolic propellants
Nigodjuk V.E., Sulinov A.V.
Problems and prospect of microgasturbines development for unmanned aerial vehicle propulsion
Zhdanov I.A., Staudacher S., Falaleev S.V.
Investigation of thermal conditions nozzle blades with a cyclone-vortex cooling system
Veretennikov S.V., Khasanov S.M.
Prospects for the forcing of gas turbine and steam power plants
Pavlova A.A.
Investigation of effects of multistage compressor final stage blading shape on compressor performance and flow pattern
Popov G.M., Krivcov A.V., Kolmakova D.A.
Mathematical models for evaluating the energy efficiency of ultralow power turbine drives
Kalabuhov D.S., Grigoryev V.A., Rad’ko V.M.
Experience of operational development of starting characteristics of the APU combustion chamber
Chechulin A.Y.
Models and methods of optimizing the procedure of measuring gas turbine engine parts using coordinate measuring devices
Bolotov M.A., Lyozin I.A.
Substantiation of the criteria for evaluation of the efficiency of the fuel supply system of the gas turbine engines
Smurova N.A.
Criteria for selecting categories of efficiency of soundproof materials used for car noise reduction
Fesina M.I., Krasnov A.V.
The analysis of real thermodynamic cycle of bypass engine with mixing
Medvedev V.V.
Analysis of temperature separation efficiency in vortex gas flows
Biryuk V.V., Kurnosov N.Y., Tarnopolsky A.V.
Common properties of hydrocarbon combustion products and Brayton cycle
Mikheenkov E.L.
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.
Methods of validation of the ballistic structure of space surveillance system orbital segment
Fadin I.A., Yanov S.V., Samokhvalov O.A.
Vortex cleaning of fuel tank pressurant gas
Biryuk V.V., Shimanov A.A., Onoprienko D.A., Smorodin A.V., Shepelev A.I.
Justification of the architecture of an interactive information model of the process of space-mission vehicle launch preparation
Privalov A.E., Bugaichenko P.Y.
Estimating the efficiency of a bypass turbojet engine on the basis of a serial gas generator as a part of the power plant of a high-altitude unmanned aerial vehicle
Zinenkov Y.V., Lukovnikov A.V., Popov A.V., Nechaev V.N.
Methods of protecting unpressurized compartments of spacecraft from the penetration of electromagnetic field
Syomkin N.D., Balakin V.L., Bragin V.V.
Estimation of functional efficiency of the air transport service system at a regional airport terminal
Koltsov I.V., Romanenko V.A.
Computation of tip clearance effect on characteristic of low pressure compressor of engine RD-33
Abdelwahid M.B., Fedorov R.M., Fedechkin K.S.
Methodological aspects of estimation foundry design and technology process efficiency for aircraft companies
Levkina O.Y.
Modeling of process energy supply and consumption of energy resources industrial enterprises
Biryuk V.V., Myatishkin G.V., Uglanov D.A., Klentak A.S.
Use of the dynamic programming method for solving tasks of GTE management optimization using the aircraft efficiency criteria
Tkachenko A.Y., Kuzmichev V.S.
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.
Designing a seal as an element of air secondary system in aircraft engines
Vinogradov A.S.
Problem of multistage compressor optimization while designing perspective gas turbine engines
Shabliy L.S.
Peculiarities of computer modeling of the working process in small gas turbine engines
Kuz'michev V.S., Tkachenko A.Y., Ostapyuk Y.A.
Improvement of efficienсy of the automated control system of nonrigid shafts surface contour in lathing
Kravchenko S.A., Nabilkin A.U., Birukov V.P.
Verification of a complex of mathematical models of aerodynamics and dynamics of Savonius rotor motion
Sizov D.A., Onushkin Y.P., Krasnova O.A., Dzhanibekov O.T.
Methods and means of accelerating particles of natural and technogenic origin
Semkin N.D., Sukhachev K.I., Dorofeev A.S.
Integrated assessment of the efficiency of an orbital inspection space system based on small satellites
Tkachenko I.S., Kaurov I.V.
Anode dissolution of a nickel-chromium alloy ЖС6У in various electrolytes
Sayapova V.V., Amirchanova N.A., Ustyuzhanina S.V., Gordeyev V.Y.
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.
Proposals for improving the efficiency and service life of the turbines of turbo-pump assemblies in liquid-propellant rocket engines by using double-sided crest-type radial labyrinth seals
Levochkin P.S., Chvanov V.K., Vasiliev V.S., Timushev S.F.
Peculiarities of Earth observation space vehicle control in contingencies
Akhmetov R.N., Makarov V.P., Sollogub A.V.
The community of the ideal and complex cycles of the gas-turbine installations
Ivanov V.A.
Experimental study of a power absorber of accelerated fluid flow in pipelines
Gimadiev M.A., Gimadiev A.G.
Theory and calculation of parameters of the detonation engine thermodynamical cycle
Grigoriev A.V., Mitrofanov V.A., Rudakov O.A., Solovieva A.V.
State of the art analysis in the automotive hybrid drives
Sinyiakov A.F., Gimadiev A.G., Ilukhin V.N., Sverbilov V.Y.
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.
Research of the mechanism of shock-inertial deposition of dispersed particles from a gas flow
Usmanova R.R., Zhernakov V.S.
Service-oriented distributed software complex for evaluation and multi-criteria analysis of reliability and survivability of on-board equipment of small satellites: Russian and Belarusian segments
Zelentsov V.A., Potryasaev S.A., Sokolov B.V., Skobtsov V.Y., Korenyako S.A., Kim D.S., Vakulchyk E.N., Kulbak L.I., Nikolaenya E.D., Lapitskaya N.V., Saksonov R.V.
Improving the efficiency of gas turbines by regenerating heat
Kulagin V.V., Sokolov M.A.
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.
Heat engine cycle limitations imposed by fuel properties
Mikheyenkov E.L.
Experimental research and selection of design parameters of the onboard microaccelerations state and compensation monitoring equipment on the low-orbit space microgravitational platform
1 1.
Increasing the capacity of engine intake system
Kozin A.M., Rusakov M.M.
Aircraft engine design based on unified gas generator
Vinogradov A.S., Parovay Y.F., Mordvinov A.G., Popov D.V., Shirokov M.A.
Assessment of technicaland economical efficiency of developing carrier rockets with first-stage reusable units
1 1., 1 1.
Research of the process of cleaning gas from mechanical impurities in a direct flow centrifugal separator
Glebov G.A., Hazbulatov A.I.
Influence of the loading parameter on the efficiency ofa three-stage turbine of turbojet bypass engine
1 1., 1 1.
On the efficiency of a radiant heating regenerative system
Panchenko V.V.
Experimental and numerical investigation of the combustion process in vortex gas burner
Yevdokimov O.A.
Research of laws of interaction of components in a liquid phase self-igniting liquid rocket fuel
1 1., 1 1.
Methodology of optimization of parameter of matching the combustion chamber and turbine joint operation
Grigoriev A.V., Golubchikov P.P., Ilushin M.Y., Rudakov O.A., Solovieva A.V.
Features of designing gas turbine of complex cycle GT24
1 1.
Pressure-gain combustion and its potential for gas turbine engine enhancement
Lutoschkin E.V., Rose M.G., Staudacher S.
Procedure of accomodation of earth remote sansing satellite external devices with regard for the satellite target operation
Akhmetov R.N., Shilov L.B., Kurenkov V.I., Yakischik A.A.
Research of toxic substances emission during water injection into a combustion chamber
Mingazov B.G., Mukhametgaliev T.H.
Preliminary study of principles of effective efficiency change of turboshaft engines of various schemes with heat recovery and intermediate cooling of working medium
Sokolov M.A., Kuzmichev V.S., Kulagin V.V., Krupenich I.N., Tkachenko A.Y.
Functional analysis of periodic disturbances during intermittent cutting
Kolodyazhny D.Y.
Some issues of research and development in aviation industry
Korchak V.Y., Kuznetsov V.V., Borisenkov I.L., Leonovich G.I., Lukachev S.V., Biryuk V.V.
The possibilities of engine volumetric efficiency increasing at the expense of self-closing inlet valve
Kozin A.M., Rusakoff M.M.
Method for calculating shipping costs in transporting heterogeneous cargo
Saveliev G.L.
Way of increase in efficiency of cycle gas turbine units
1 1.
1 - 78 of 78 Items

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