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Title
Authors
Method of design calculation jet-centrifugal gas-liquid duplex fuel nozzle with internal mixing
Egorychev V.S.
The flowing reactor as the tool of an experimental research of processes of transformation self-igniting liquid rocket fuel
1 1., 1 1.
Method of design calculation gas-liquid jet duplex fuel nozzle with internal mixing
Egorychev V.S.
Study of the efficiency of the application of gas dynamic stabilization of the flame in a current engine
Belonozhkin V.V., Teslya D.N.
Мethod of design calculation of centrifugal emulsive duplex fuel nozzle
1 1.
Increasing the overall performance of a two-stroke engine with spark ignition by fuel injection
Dovgyallo A.I., Krasheninnikov S.V., Shchepetov D.A.
Quasi one-dimensional model and calculation of processes in gas turbineengine combustion chambers given the heterogeneity of the combustible mixture, changes in mass, composition, temperature and stirring efficiency of the working body
Didenko A.A., Sokolov A.B.
Analysis estimation of pulse jet engine operation in detonation mode
Seyfetdinov R.B., Seyfetdinov M.B., Gafurov S.A., Shakhmatov E.V.
Optoelectronic device for the control of hydrocarbon fuel cavitation treatment
1 1.
Results of experimental studies of parameters of low-thrust rocket engines operating on gaseous oxygen-hydrogen fuel
Ageenko Y.I., Lapshin E.A., Morozov I.I., Pegin I.V., Ryzhkov V.V.
Design and investigation of a pneumatic atomizer as applied to a low emission combustion chamber of a promising gas-turbine engine
Vasilyev A.Y., Chelebyan O.G., Yagodkin V.I.
Cycle parameters of an internal combustion spark-ignition gas piston engine with an electronic control system
Shishkov V.A.
Limit values of the Brayton cycle with the use of reduced fuel characteristics
Mikheenkov E.L., Nekrasova S.O.
Prospects and problems of movement and power plants in powder metal fuel
Egorov A.G., Tizilov A.S.
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.
Mathematical model of fuel sloshing in the measuring channel of the fuel expenditure control system
Kryukov Y.A.
Method of reduced fuel characteristics and parameters of the operating cycles of heat engines
Anastaseev V.V., Belozertsev S.V., Mikheenkov E.L., Nekrasova S.O.
Optimal command control of hypersonic aircraft flight path in conditions of atmospheric disturbances
Krikunov M.M.
Joint work of units and characteristics of elements gas the equipment for the engine of internal combustion with spark ignition
Shishkov V.A., Lesnih U.I.
Experimental and numerical investigation of the combustion process in vortex gas burner
Yevdokimov O.A.
Analysis of control programs and flight paths of a hypersonic vehicle in climb
Balakin V.L., Krikunov M.M.
Estimation of the required thrust impulse for small spacecraft (SSC) control system with a propulsion system using fuel gas components
Titov B.A., Koltsov I.V.
Study of characteristics of the launch vehicle fuel line gas damper
Gimadiev A.G., Odinokov D.A., Stadnik D.M., Greshnyakov P.I.
On plasma support of fuel burning in a combustion chamber of a gas-turbine facility
Bulaeva M.N., Kravchenko I.V., Riaby V.A., Tkachenko D.P.
Using the energy of gas differential pressure in electromagnetic injectors for improved breathing of spark-ignition internal combustion engine cylinders
Shishkov V.A.
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.
Method of pipeline system designing taking into account complex interaction of static and dynamic processes with strength characteristics
Mironova T.B., Prokofiev A.B., Rodionov L.V.
Сalculated analysis of the influence of operation and design factors on the parameters of oxygen-hydrogen low-thrust rocket engines
Ryzhkov V.V., Morozov I.I.
Improving the efficiency of diesel engines by means of electroprocessing of fuel
Kozmenkov I.N., Nosyrev D.Y.
Choosing the mixing pattern for oxygen-hydrogen low-thrust rocket engines
Ryzhkov V.V., Morozov I.I.
Relationship between carbon concentration in a fuel and characteristics of flame propagation with a magnitude of ion current
Shaykin A.P., Budaev S.I., Galiev I.R.
Estimation of mass-dimensional characteristics of a complex propulsion unit of earth remote sensing spacecraft
Kurenkov V.I., Kucherov A.S., Yakishik A.A.
Robust research of the fuzzy logic controllers using a fuel flow control loop of the gas-turbine engine as an example
Chicherova E.V.
Quality indices of an internal combustion engine controlled by the discharge current channel
1 1., 1 1., 1 1.
Research of laws of interaction of components in a liquid phase self-igniting liquid rocket fuel
1 1., 1 1.
Experimental research of wall boundary flow formation in the combustion chamber of a small gas generator with self-igniting fuel components
Shustov S.A.
Peculiarities of starting a spark-ignition gas fuel internal combustion engine
Shishkov V.A.
Energy sources in heat engine cycles
Mikheyenkov E.L.
Development of elements and parameters of LNG fuel system with cryogenic piston pump and gas receiver for road gas turbine locomotive
Bukin V.A., Rudenko V.F.
Development of a procedure for the synthesis of a micro gas turbine engine neural controller with account for fuel consumption constraints
Kuznetsov A.V., Makaryants G.M.
Significance and directions of development of rotary piston area of research
Okorochkov V.V., Okorochkova V.M., Shafranov V.V.
Determining the angle of advance of ignition when switching from petrol to gas depending on fuel mixture burning rate
Shishkov V.A.
Results of primary operation of NK-37 engine low emission combustion system
Bantikov D.Y., Yeliseev Y.S., Lavrov V.N., Pchelyakov A.A., Fedorchenko D.G., Tsybizov Y.I.
Simulation of drop coagulations in swirled time dependent streams with reference to gas turbine engine combustion chambers
Sviridenkov A.A., Tretyakov V.V.
Operation of an electronic system of control for spark-ignition gas fuel internal combustion engines in ignition misses
Shishkov V.A.
Heat engine cycle limitations imposed by fuel properties
Mikheyenkov E.L.
On selection of automatic control system for crvogenic fuel gas turbine engine
Bukin V.A.
Development and research of a device for gas sheet stamping with a piston pressure multiplier
Botashev A.Y., Bayramukov R.A.
A new mathematical tool for modelling the processes in fuel sprays
Sazhin S.S., Sobolev V.A., Shchepakina E.A.
Model of sedimentation of solid particles of heterogeneous materials
Polyanskov Y.V., Evseev A.N., Poroykov V.A.
Thermodynamic shape of the combined power installations, based on GTU and solid oxide fuel cells
Loskutnikov A.A., Gorjunov I.M., Bakirov F.G.
Determining the interrelation between detonation characteristics indicators and electrodynamic parameters of hydrocarbon fuels on the basis of statistical modelling of componental structure
1 1., 1 1., 1 1.
Mathematical model of small-thrust rocket engine with gaseous oxygen and hydrogen in pulse operation
1 1.
Applying the possibilities of Microsoft Excel for solving problems of fuel burning thermodynamics
Mikheenkov E.L., Nekrasova S.O., Ramzaeva E.A.
Issues of evolution of rotor piston engines’ subject abroad and in Russia
Kocherov E.P., Kononov V.A., Okorochkov V.V., Okorochkova V.M., Ivanova K.P.
Technology of computational analysis of the working process parameters of low-thrust rocket engines running on gaseous oxygen-hydrogen fuel with the use of ANSYS CFD
Ryzhkov V.V., Morozov I.I.
Metrological analysis of a device rof nondestructive control of flight vehicle fuel tank current conductive coatings
Samsonov A.S., Blinov D.I., Skvortsov B.V., Zhivonosnovskaya D.M.
Numerical simulation of gas temperature spatial distribution in a one-burner sector of a gas turbine combustor with uncertain initial conditions of fuel atomization
Kostyuk V.Y., Kirilash Y.I., Stasyuk A.V., Shein V.V., Karzov D.V.
Progressive thermodynamic cycle of internal combustion engine based on сrank a rod the mechanism with dual kinematic communications
Grabovskiy A.A.
Defining the specific impulse of mixed solid propellants
1 1., 1 1.
Specific features of pressure pulsation control in combustion chambers of land based gas turbine units
Skiba D.V., Maksimov D.A., Kashapov R.S., Kharisov T.S.
Working process of gaseous fuel metallizator
Pervyshin A.N., Ryazanov A.I.
Disturbed motion of a hypersonic vehicle in climb
Balakin V.L., Krikunov M.M.
Fluctuations of liquid fuel in tanks with oil recovery units
Dyachenko M.I., Duy Hung N., Temnov A.N.
Experience of operational development of starting characteristics of the APU combustion chamber
Chechulin A.Y.
Modeling dynamic processes of response of fuel pressure-operated valves of superheavy launch vehicles in the tasks of providing structural strength
Sazanov V.P., Chirkov A.V.
Command control of hypersonic cruising aircraft during climb
Balakin V.L., Kotchyan A.G.
Guaranteeing of ecological and economic indicators of internal combustion engine
Grabovskiy A.A., Mironov V.A.
Development of advanced low thrust rocket engines with ecologically friendly propellants
1 1., 1 1., 1 1.
The mixing efficiency of liquid droplet fuel and air flow in the frontal swirl devices
1 1., 1 1.
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.
Test bench for investigation of thrusters intra-chamber working processes
Pervyshin A.N., Ryazanov A.I.
Possibility of use of passing gases in gasturbine engines created within the limits of conversion
Rosljakov A.D., Kocherov E.P., Tsibizov J.I.
Theoretical and experimental studies of a gas stamping device with a piston pressure multiplier
Botashev A.Y., Bayramukov R.A.
Characteristics of a fuel spray downstream the pressure atomizers under high pressure in the combustion chamber
Sviridenkov A.A., Tretyakov V.V.
Common properties of hydrocarbon combustion products and Brayton cycle
Mikheenkov E.L.
State of the art analysis in the automotive hybrid drives
Sinyiakov A.F., Gimadiev A.G., Ilukhin V.N., Sverbilov V.Y.
Approaches to the evaluation of fuels for hypersonic engines
Sergeev S.M., Petrukhin N.V.
The combined fuel draining control system for liquid oxygen and liquid hydrogen upper stage
Ivanov V.P., Partola I.S.
Manipulate pulsed detonation engine
1 1., 1 1.
The algorithm of calculation combined energy installations, based on turbojet and SOFC
Loskutnikov A.F., Bakirov F.G., Gorjunov I.M.
Modeling direct fuel injection by a multipin nozzle into the ice combustion chamber using CAE/CAD-systems
Biryuk V.V., Kayukov S.S., Gorshkalev A.A., Uglanov D.A., Lysenko Y.D., Zvyagintsev V.A.
Improving the efficiency of the powerplant of an unmanned aerial vehicle through the use of cryogenic fuel
Kolesnikov A.S., Grasko T.V., Raznoschikov V.V.
Features of start-up the engine of internal combustion with spark ignition on gas fuel
Shishkov V.A.
Turboprofan jet modeling and equivalent specific fuel consumption optimization subsystem construction on the seminatural modelling stand
Pogorelov G.I., Krivosheev I.A., Godovanyuk A.G., Danilin O.E., Badamshin B.I.
Optimization of fuel distribution in the afterburner of a gas turbine engine
Nelyubin V.R.
Experimental study of free-convection flame propagation
Yevdokimov O.A., Guryanov A.I.
Fluctuations of pressure in rail gas injection of engines with spark ignition
Shishkov V.A.
Evaluation of the possibility of using combustion promoters in hydrocarbon fuels for perspective jet engines
Petrukhin N.V., Sergeev S.M., Prokopenko O.A., Grek M.O.
Algorithm of adaptation of an electronic control system of internal combustion engines to various chemical compositions of gas fuel
Shishkov V.A.
The simplification of heat engines thermodynamics calculation with using of idaeal gas’ model
1 1., 1 1.
Optimal control of the angle of attack of a hypersonic flight vehicle
Bebyakov A.A.
1 - 92 of 92 Items

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