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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)

Problems and prospect of microgasturbines development for unmanned aerial vehicle propulsion

Zhdanov I.A., Staudacher S., Falaleev S.V.

(Rus)

Vol 10, No 2 (2011)

Construction of a blade beam finite element as a component of the blade disk rotary-symmetrical system

Davydov D.P.

(Rus)

Vol 9, No 4 (2010)

Development of turbopump unit design for hydrogen liquid-propellant rocket engines without generators developed at the design bureau of chemical automation

Dmitrenko A.I., Ivanov A.V., Rachuk V.S.

(Rus)

Experimental development of the LRE with CCCM nozzle’s extension

(Rus)

Laws of life dispersion and statistical estimation of life distribution boundaries as applied to aviation engine LPC disks

Kutyrev V.V., Teplova S.V.

(Rus)

Pressure-gain combustion and its potential for gas turbine engine enhancement

Lutoschkin E.V., Rose M.G., Staudacher S.

(Rus)

Vol 12, No 2 (2013)

Investigation of energy parameters of small-thrust liquid rocket engines with the geometric expansion ratio of the nozzle F=200

Ageenko Y.I., Nigodyuk V.E., Ryzhkov V.V., Sulinov A.V., Shustov S.A.

(Rus)

Vol 20, No 3 (2021)

Experimental studies of the components of high-frequency ion engine RD0310

Kazbanov A.A., Dronov P.A., Spivak O.O., Derkachev A.B.

(Rus)

Vol 19, No 2 (2020)

Gas turbine engine dynamic model based on variable-memory LSTM architecture

Kuznetsov A.V., Makaryants G.M.

(Rus)

Vol 10, No 6 (2011)

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

Shishkov V.A.

(Rus)

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

The determination of the thermoacoustic generator aspect from electrodynamic unit features by the parametric-studies

Vorotnikov G.V., Kruchkov A.N., Zynovyev E.A.

(Rus)

Internal combustion engine some cooling system components detailed calculation

Kolomin I.V., Ajukov A.A., Birjuk V.V.

(Rus)

Vol 10, No 3-2 (2011): Special Issue

The numerical modelling of processes in combustion chambers of low thrust rocket engines

Salich V.L.

(Rus)

Vol 18, No 1 (2019)

Influence of the stressed state of the surface layer on the endurance of gas turbine engine compressor blades

Sazonov M.B., Solovatskaya L.V.

(Rus)

Vol 17, No 4 (2018)

Оptimization of gas turbine aircraft engine control throughout the engine service life

Gurevich O.S., Golberg F.D., Smetanin S.A., Trifonov M.E.

(Rus)

Vol 17, No 3 (2018)

Refining methods of vibration diagnostics of wear of turbo-prop engine differential speed reduction unit gear teeth

Avramenko A.A., Kryuchkov A.N., Plotnikov S.M., Sundukov E.V., Sundukov A.E.

(Rus)

Vol 16, No 3 (2017)

Constructing 3D fan blade models in CAD-system on the basis of coordinate measuring techniques

Arkhipov A.N., Ravikovich Y.A., Fedorov I.M., Kholobtsev D.P.

(Rus)

Vol 15, No 4 (2016)

Research of liquid outflow from low-emission swirl injectors of a low-thrust liquid rocket engine

Semkin Y.V.

(Rus)

Vol 15, No 1 (2016)

Efficiency of using electric propulsion engines for the task of keeping in a near-circular orbit

Ishkov S.A.

(Rus)

Vol 14, No 3-1 (2015): Special Issue

Modification of the starter turbine disk for blade containment certification tests

Karimbaev K.D., Sapronov D.V.

(Rus)

Vol 14, No 1 (2015)

Vortex cleaning of fuel tank pressurant gas

Biryuk V.V., Shimanov A.A., Onoprienko D.A., Smorodin A.V., Shepelev A.I.

(Rus)

Vol 13, No 5-4 (2014): Special Issue

Examination of the theoretical possibility of creating a vernier electrorocket engine

Baigaliev B.E., Chernoglazova A.V., Tumakov E.A., Temnikova S.V.

(Rus)

Vol 13, No 5-2 (2014): Special Issue

Development of a single-section demonstrator rotary engine on the basis of a modern complex design procedure

Kostyuchenkov A.N., Zelentsov A.A., Semenov P.V., Minin V.P.

(Rus)

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

Research of the influence of design parameters of a 400 N-thrust low-thrust liquid rocket engine on its energy efficiency

Ageenko Y.I., Ilyin R.V., Pegin I.V.

(Rus)

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

A simplified method of thermoacoustic engine analysis

Zynovyev E.A., Dovgyallo A.I.

(Rus)

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

The task of creating the bypass engines of various thrust levels using the given gas generator

Kocherov E.P., Kuzmichev V.S., Kulagin V.V., Fedorchenko D.G.

(Rus)

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

Investigation of the possibility of the creation LREST by thrust 400 N with a baffle - centrifugal scheme of NT and NDMG mixing

Ageenko Y.I., Ilin I.V., Pegin I.V., Shalamov E.A.

(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)

Optimal distribution of turboprop engine free energy between the screw and the jet with mass characteristics taken into account

Grigoriev V.A., Prokaev A.S.

(Rus)

Modelling of an ejector for turbine aeroengines for application in performance synthesis tools

Georgi J., Staudacher S., Falaleev S.V.

(Rus)

Vol 10, No 2 (2011)

Some results of experimental refining of a constant volume valve combustion chamber

Bogdanov V.I., Kuznetsov S.P.

(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)

Development of advanced low thrust rocket engines with ecologically friendly propellants

1 1., 1 1., 1 1.

(Rus)

Vol 8, No 3-2 (2009): Special Issue

Мethod of design calculation of centrifugal emulsive duplex fuel nozzle

1 1.

(Rus)

Improvement of a design piston of diesel engine of tractor

Rogdestvensky Y.V., Doykin A.A., Murzin V.S.

(Rus)

Vol 8, No 2 (2009)

Dependence of the extent to which the space vehicle’s own atmosphere and plasma generated by stationary plasma engines affect the space vehicle on its structural lay-out

Testoyedov N.A., Smirnov V.A.

(Rus)

Vol 12, No 3-1 (2013): Vestnik SSAU

Characteristics of the sampling instrument for measuring emissions of an aircraft gas turbine engine

Okhlobystin A.V., Lyubimov R.V., Sokolova N.N.

(Rus)

Vol 21, No 1 (2022)

Increasing the sensitivity and expanding the functionality of bipolar analysis of rotary machine vibrations

Sundukov A.E., Shakhmatov Y.V.

(Rus)

Vol 19, No 1 (2020)

Using signals from the gas-turbine engine shaft speed sensor in the diagnosis of the technical condition of its reduction gearbox

Avramenko A.A., Kryuchkov A.N., Plotnikov S.M., Sundukov E.V., Sundukov A.E.

(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)

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

Harmonic model of thermodynamic cycle in thermoacoustic engine regenerator

Zynovyev E.A., Dovgyallo A.I., Vorotnikov G.V.

(Rus)

Aircraft engine design based on unified gas generator

Vinogradov A.S., Parovay Y.F., Mordvinov A.G., Popov D.V., Shirokov M.A.

(Rus)

Vol 10, No 3-2 (2011): Special Issue

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

Bukin V.A.

(Rus)

Vol 18, No 1 (2019)

Influence of the geometry fidelity of resonant sound-absorbing liner samples on their acoustic characteristics

Kustov O.Y., Khramtsov I.V., Bulbovich R.V.

(Rus)

Vol 17, No 4 (2018)

Theory and calculation of parameters of the detonation engine thermodynamical cycle

Grigoriev A.V., Mitrofanov V.A., Rudakov O.A., Solovieva A.V.

(Rus)

Vol 17, No 2 (2018)

Improvement of friction units of power plants by aplying ceramic composite spray coatings

Siluyanova M.V., Fertikov A.O.

(Rus)

Vol 16, No 2 (2017)

Multi-purpose high-precision thermal vacuum testing bench and someresults of firing tests of non-hypergolic low-thrust rocket engines

Ryzhkov V.V., Verjasov Y.N., Galperin R.N., Gulyaev Y.I., Ivashin Y.S.

(Rus)

Vol 15, No 4 (2016)

Method of vibration diagnostics of aerodynamic and aeroelastic oscillations in gas turbine engine compressor

Posadov V.V., Remizov A.E.

(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 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 14, No 1 (2015)

Computer-aided design of aircraft gas turbine engines and selection of materials for their main parts

Akhmedzyanov D.A., Kishalov A.E., Markina K.V.

(Rus)

Vol 13, No 5-4 (2014): Special Issue

11D58MF combined propulsion unit operating on oxygen-hydrogen fuel for an average-sized booster

Lupyak D.S., Smolentsev A.A., Sokolov B.A., Tumanin E.N., Tupitsin N.N.

(Rus)

Vol 13, No 5-2 (2014): Special Issue

Investigation of 11D428А-22 thruster operation dynamics with bellows flow stabilizer

Beshenev Y.A., Volkov A.V., Kazankin F.A.

(Rus)

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

50 n thrust correction engine for the "Luna-resurs" lunar module descent engine

Ageenko Y.I., Pegin I.V., Chesnokov D.V.

(Rus)

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

The modeling of the thermoacoustic electric generator by quadrupole approximation approach

Vorotnikov G.V.

(Rus)

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

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.

(Rus)

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

About some directions in development avation engine buildings

Zamtfort B.S.

(Rus)

Aerodynamic improvement of GTE compressors by space profiling of blade vanes

Gerasimenko V.P., Shelkovsky M.Y.

(Rus)

Improving the quality parameters of serial debug two spool mixed flow turbofan

Volik A.A., Gumerov K.S., Khabibullin R.Z., Khayrullin R.B.

(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 9, No 1 (2010)

The influence of operational and technological factors on the dynamic parameters of elastic elements of elastic damping rotor supports

1 1., 1 1., 1 1.

(Rus)

Manipulate pulsed detonation engine

1 1., 1 1.

(Rus)

Vol 8, No 3-2 (2009): Special Issue

Feature of optimization of parameters of working process GTE with the free turbine at initial designing in the conditions of uncertainty

1 1., 1 1.

(Rus)

About the thermal protection of the oil cavities for designing gas turbine engines

Tryanov A.Y., Grishanov O.A., Vinogradov A.S.

(Rus)

Vol 8, No 2 (2009)

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.

(Rus)

Vol 12, No 3-1 (2013): Vestnik SSAU

Test case of 3d unsteady swirling flows modeling using commercial and in-house codes

Nazukin V.A., Avgustinovich V.G., Thornber B., Aguado Lopez P., Tsatiashvili V.V., Koromyslov E.V.

(Rus)

Vol 21, No 3 (2022)

Diagnostic indicators of tooth flank wear based on the analysis of tooth spectral component parameters

Sunduckov A.E.

(Rus)

Vol 20, No 4 (2021)

The structure of knowledge base to support the development of low-thrust liquid-propellant rocket engines based on computer technologies

Ryzhkov V.V.

(Rus)

Vol 20, No 1 (2021)

Mathematical model of turbofan engine weight estimation taking into account the engine configuration and size

Avdeev S.V.

(Rus)

Vol 18, No 4 (2019)

Simulation model of oscillations of the “sun gear – satellites” pair of turboprop engine planetary reduction gearbox in the presence of defects of tooth flanks

Kryuchkov A.N., Plotnikov S.M., Sundukov E.V., Sundukov A.E.

(Rus)

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

Efficiency of technical workings out in batch production GTE

Aleksentsev E.I., Shitarev I.L., Kurbatov V.P., Gritsenko E.A.

(Rus)

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

Shishkov V.A.

(Rus)

Numerical study of possibility of reliable diagnostics of gas turbine engine by gasdynamic parameters using a linear mathematical model

Gerasimov A.B., Sundukov M.Y.

(Rus)

Vol 10, No 3-2 (2011): Special Issue

Research of the postoperational condition of the restored compressor shovels of GTD gas-transfer of the units which have fulfilled the appointed resource

Tarasenko Y.P., Tsareva I.N., Krivina L.A.

(Rus)

Vol 18, No 1 (2019)

Research of the operability of an air-fuel lubrication and cooling system of gas turbine engine rotor bearings

Klimov V.N., Dud’ev D.Y., Sigaylo V.Y., Klimov N.I., Mashkov Y.K.

(Rus)

Vol 17, No 4 (2018)

Automated construction of a fan blade model according to data of CAD profile measurements

Arkhipov A.N., Bugrjashova E.V., Ravikovich Y.A., Savin R.A., Terentjev V.V., Shevjakov A.O.

(Rus)

Vol 17, No 2 (2018)

Determination of large-size liner impedance based on numerical simulation of sound propagation in a duct with specified azimuthal modal structure

Korin I.A., Palchikovskiy V.V., Pavlogradskiy V.V.

(Rus)

Vol 16, No 2 (2017)

Assessment of gas turbine engine airfoil surface microstructure

Nosov N.V., Abramov A.D., Kosulin S.I.

(Rus)

Vol 15, No 4 (2016)

Peculiarities of computer modeling of the working process in small gas turbine engines

Kuz'michev V.S., Tkachenko A.Y., Ostapyuk Y.A.

(Rus)

Vol 14, No 4 (2015)

Investigation of the causes of crack origination in the inner casing of NK-86 gas turbine engine combustion chamber

Kocherova Е.Е.

(Rus)

Vol 10, No 5 (2011)

Analysis of the properties of water condensate obtained from heat engine exhaust yases

Knysh Y.A., Uglanov D.A.

(Rus)

Vol 14, No 1 (2015)

Development of a solar battery orientation robot system for small spacecraft

Beznyakov A.M., Vlasov V.A., Malenin E.N.

(Rus)

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

Development of the technology of diagnostics of turbo-jet aviation engines by a filtering element with a diagnostic layer

Drokov V.V., Drokov V.G., Muryshenko V.V., Mukhutdinov F.I., Khaliullin V.F.

(Rus)

Vol 13, No 5-2 (2014): Special Issue

Research of gas turbine engine operation in dust-filled atmosphere

Abdullin B.R., Akmaletdinov R.G., Goumerov K.S., Nigmatullin R.R.

(Rus)

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

Experimental verification of the possibility of improving the liquid propelant rocket engine performance for the “Vega” launcher upper stage

Kovalenko A.N., Pereverzev V.G., Marchan R.A., Blishun Y.V.

(Rus)

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

The calculation of optimum worker frequencies of the thermoacoustic electric generator with including ready electrodynamic unit and given load

Vorotnikov G.V., Kryuchkov A.N.

(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)

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

Methods of increase of wear resistance and vibroakusticheskikh of parameters of knots of the friction of space equipment

Gromakovsky D.G., Kovshov A.G., Kotcherov E.P., Makaryants M.V.

(Rus)

Vol 11, No 5-1 (2012): Special Issue

Use of the dynamic programming method for solving tasks of GTE management optimization using the aircraft efficiency criteria

Tkachenko A.Y., Kuzmichev V.S.

(Rus)

Method of calculating GTE gas-thermodynamic parameters with blade row description of an axial multistage compressor

Boyko L.G., Karpenko E.L., Akhtemenko U.F.

(Rus)

Definition of overall limits internal-combustion engine using vector modeling

Kosenok B.B.

(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)

1 1., 1 1.

(Rus)

Theoretical calculation approach of gas turbine engines compressor characteristic line

1 1.

(Rus)

Vol 8, No 3-2 (2009): Special Issue

The efficiency of aligning gratings at engine inlet of ground power plants

(Rus)