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Method of design calculation jet-centrifugal gas-liquid duplex fuel nozzle with internal mixing

Egorychev V.S.

(Rus)

The flowing reactor as the tool of an experimental research of processes of transformation self-igniting liquid rocket fuel

1 1., 1 1.

(Rus)

Method of design calculation gas-liquid jet duplex fuel nozzle with internal mixing

Egorychev V.S.

(Rus)

Vol 22, No 3 (2023)

Study of the efficiency of the application of gas dynamic stabilization of the flame in a current engine

Belonozhkin V.V., Teslya D.N.

(Rus)

Мethod of design calculation of centrifugal emulsive duplex fuel nozzle

1 1.

(Rus)

Prospects and problems of movement and power plants in powder metal fuel

Egorov A.G., Tizilov A.S.

(Rus)

Vol 20, No 2 (2021)

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.

(Rus)

Vol 15, No 1 (2016)

Mathematical model of fuel sloshing in the measuring channel of the fuel expenditure control system

Kryukov Y.A.

(Rus)

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.

(Rus)

Increasing the overall performance of a two-stroke engine with spark ignition by fuel injection

Dovgyallo A.I., Krasheninnikov S.V., Shchepetov D.A.

(Rus)

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.

(Rus)

Vol 10, No 5 (2011)

Analysis estimation of pulse jet engine operation in detonation mode

Seyfetdinov R.B., Seyfetdinov M.B., Gafurov S.A., Shakhmatov E.V.

(Rus)

Vol 9, No 1 (2010)

Optoelectronic device for the control of hydrocarbon fuel cavitation treatment

1 1.

(Rus)

Vol 23, No 3 (2024)

Development and research testing of a low thrust on gaseous-propellant rocket engine chamber

Musteikis A.I., Levikhin A.A., Kolosenok S.V.

(Rus)

Vol 13, No 5-3 (2014): Special Issue

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.

(Rus)

Vol 10, No 5 (2011)

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.

(Rus)

Vol 13, No 5-1 (2014): Special Issue

Cycle parameters of an internal combustion spark-ignition gas piston engine with an electronic control system

Shishkov V.A.

(Rus)

Limit values of the Brayton cycle with the use of reduced fuel characteristics

Mikheenkov E.L., Nekrasova S.O.

(Rus)

Vol 20, No 4 (2021)

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.

(Rus)

Vol 10, No 3-4 (2011): Special Issue

Working process of gaseous fuel metallizator

Pervyshin A.N., Ryazanov A.I.

(Rus)

Vol 18, No 2 (2019)

Disturbed motion of a hypersonic vehicle in climb

Balakin V.L., Krikunov M.M.

(Rus)

Vol 16, No 2 (2017)

Fluctuations of liquid fuel in tanks with oil recovery units

Dyachenko M.I., Duy Hung N., Temnov A.N.

(Rus)

Vol 14, No 2 (2015)

Experience of operational development of starting characteristics of the APU combustion chamber

Chechulin A.Y.

(Rus)

Vol 11, No 4 (2012)

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.

(Rus)

Vol 11, No 1 (2012)

Command control of hypersonic cruising aircraft during climb

Balakin V.L., Kotchyan A.G.

(Rus)

Guaranteeing of ecological and economic indicators of internal combustion engine

Grabovskiy A.A., Mironov V.A.

(Rus)

Vol 8, No 3-3 (2009): Special Issue

Development of advanced low thrust rocket engines with ecologically friendly propellants

1 1., 1 1., 1 1.

(Rus)

The mixing efficiency of liquid droplet fuel and air flow in the frontal swirl devices

1 1., 1 1.

(Rus)

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.

(Rus)

Vol 10, No 3-4 (2011): Special Issue

Test bench for investigation of thrusters intra-chamber working processes

Pervyshin A.N., Ryazanov A.I.

(Rus)

Possibility of use of passing gases in gasturbine engines created within the limits of conversion

Rosljakov A.D., Kocherov E.P., Tsibizov J.I.

(Rus)

Vol 18, No 1 (2019)

Theoretical and experimental studies of a gas stamping device with a piston pressure multiplier

Botashev A.Y., Bayramukov R.A.

(Rus)

Vol 15, No 4 (2016)

Characteristics of a fuel spray downstream the pressure atomizers under high pressure in the combustion chamber

Sviridenkov A.A., Tretyakov V.V.

(Rus)

Vol 14, No 1 (2015)

Common properties of hydrocarbon combustion products and Brayton cycle

Mikheenkov E.L.

(Rus)

Vol 11, No 3-3 (2012): Special Issue

State of the art analysis in the automotive hybrid drives

Sinyiakov A.F., Gimadiev A.G., Ilukhin V.N., Sverbilov V.Y.

(Rus)

Approaches to the evaluation of fuels for hypersonic engines

Sergeev S.M., Petrukhin N.V.

(Rus)

The combined fuel draining control system for liquid oxygen and liquid hydrogen upper stage

Ivanov V.P., Partola I.S.

(Rus)

Vol 8, No 3-3 (2009): Special Issue

Manipulate pulsed detonation engine

1 1., 1 1.

(Rus)

Vol 8, No 3-1 (2009): Special Issue

The algorithm of calculation combined energy installations, based on turbojet and SOFC

Loskutnikov A.F., Bakirov F.G., Gorjunov I.M.

(Rus)

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.

(Rus)

Vol 19, No 3 (2020)

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.

(Rus)

Features of start-up the engine of internal combustion with spark ignition on gas fuel

Shishkov V.A.

(Rus)

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.

(Rus)

Vol 17, No 4 (2018)

Optimization of fuel distribution in the afterburner of a gas turbine engine

Nelyubin V.R.

(Rus)

Vol 14, No 1 (2015)

Experimental study of free-convection flame propagation

Yevdokimov O.A., Guryanov A.I.

(Rus)

Vol 11, No 3-2 (2012): Special Issue

Fluctuations of pressure in rail gas injection of engines with spark ignition

Shishkov V.A.

(Rus)

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.

(Rus)

Vol 10, No 1 (2011)

Algorithm of adaptation of an electronic control system of internal combustion engines to various chemical compositions of gas fuel

Shishkov V.A.

(Rus)

Vol 8, No 3-3 (2009): Special Issue

The simplification of heat engines thermodynamics calculation with using of idaeal gas’ model

1 1., 1 1.

(Rus)

Vol 12, No 1 (2013)

Optimal control of the angle of attack of a hypersonic flight vehicle

Bebyakov A.A.

(Rus)

Vol 19, No 1 (2020)

Optimal command control of hypersonic aircraft flight path in conditions of atmospheric disturbances

Krikunov M.M.

(Rus)

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.

(Rus)

Experimental and numerical investigation of the combustion process in vortex gas burner

Yevdokimov O.A.

(Rus)

Vol 17, No 4 (2018)

Analysis of control programs and flight paths of a hypersonic vehicle in climb

Balakin V.L., Krikunov M.M.

(Rus)

Vol 10, No 6 (2011)

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.

(Rus)

Vol 14, No 1 (2015)

Study of characteristics of the launch vehicle fuel line gas damper

Gimadiev A.G., Odinokov D.A., Stadnik D.M., Greshnyakov P.I.

(Rus)

Vol 11, No 3-1 (2012): Special Issue

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.

(Rus)

Vol 10, No 1 (2011)

Using the energy of gas differential pressure in electromagnetic injectors for improved breathing of spark-ignition internal combustion engine cylinders

Shishkov V.A.

(Rus)

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.

(Rus)

Vol 12, No 2 (2013)

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.

(Rus)

Vol 18, No 3 (2019)

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.

(Rus)

Improving the efficiency of diesel engines by means of electroprocessing of fuel

Kozmenkov I.N., Nosyrev D.Y.

(Rus)

Vol 17, No 3 (2018)

Choosing the mixing pattern for oxygen-hydrogen low-thrust rocket engines

Ryzhkov V.V., Morozov I.I.

(Rus)

Vol 14, No 4 (2015)

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.

(Rus)

Vol 13, No 5-3 (2014): Special Issue

Estimation of mass-dimensional characteristics of a complex propulsion unit of earth remote sensing spacecraft

Kurenkov V.I., Kucherov A.S., Yakishik A.A.

(Rus)

Vol 11, No 3-1 (2012): Special Issue

Robust research of the fuzzy logic controllers using a fuel flow control loop of the gas-turbine engine as an example

Chicherova E.V.

(Rus)

Vol 9, No 1 (2010)

Quality indices of an internal combustion engine controlled by the discharge current channel

1 1., 1 1., 1 1.

(Rus)

Research of laws of interaction of components in a liquid phase self-igniting liquid rocket fuel

1 1., 1 1.

(Rus)

Vol 12, No 2 (2013)

Experimental research of wall boundary flow formation in the combustion chamber of a small gas generator with self-igniting fuel components

Shustov S.A.

(Rus)

Vol 10, No 6 (2011)

Peculiarities of starting a spark-ignition gas fuel internal combustion engine

Shishkov V.A.

(Rus)

Energy sources in heat engine cycles

Mikheyenkov E.L.

(Rus)

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.

(Rus)

Vol 17, No 3 (2018)

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.

(Rus)

Vol 13, No 5-3 (2014): Special Issue

Significance and directions of development of rotary piston area of research

Okorochkov V.V., Okorochkova V.M., Shafranov V.V.

(Rus)

Vol 11, No 2 (2012)

Determining the angle of advance of ignition when switching from petrol to gas depending on fuel mixture burning rate

Shishkov V.A.

(Rus)

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.

(Rus)

Simulation of drop coagulations in swirled time dependent streams with reference to gas turbine engine combustion chambers

Sviridenkov A.A., Tretyakov V.V.

(Rus)

Vol 10, No 6 (2011)

Operation of an electronic system of control for spark-ignition gas fuel internal combustion engines in ignition misses

Shishkov V.A.

(Rus)

Heat engine cycle limitations imposed by fuel properties

Mikheyenkov E.L.

(Rus)

On selection of automatic control system for crvogenic fuel gas turbine engine

Bukin V.A.

(Rus)

Vol 17, No 2 (2018)

Development and research of a device for gas sheet stamping with a piston pressure multiplier

Botashev A.Y., Bayramukov R.A.

(Rus)

Vol 10, No 5 (2011)

A new mathematical tool for modelling the processes in fuel sprays

Sazhin S.S., Sobolev V.A., Shchepakina E.A.

(Rus)

Vol 11, No 2 (2012)

Model of sedimentation of solid particles of heterogeneous materials

Polyanskov Y.V., Evseev A.N., Poroykov V.A.

(Rus)

Thermodynamic shape of the combined power installations, based on GTU and solid oxide fuel cells

Loskutnikov A.A., Gorjunov I.M., Bakirov F.G.

(Rus)

Vol 9, No 1 (2010)

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.

(Rus)

Mathematical model of small-thrust rocket engine with gaseous oxygen and hydrogen in pulse operation

1 1.

(Rus)

Applying the possibilities of Microsoft Excel for solving problems of fuel burning thermodynamics

Mikheenkov E.L., Nekrasova S.O., Ramzaeva E.A.

(Rus)

Vol 10, No 3-4 (2011): Special Issue

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.

(Rus)

Vol 18, No 2 (2019)

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.

(Rus)

Vol 16, No 3 (2017)

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.

(Rus)

Vol 11, No 2 (2012)

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.

(Rus)