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Vol 23, No 2 (2024)

Method of first-approximation calculation of take-off weight of a light aircraft with a hybrid propulsion system

Sychev A.V., Arbuzov I.V., Ravikovich Y.A.

(Rus)

Vol 23, No 2 (2024)

Increasing the efficiency and stability of fuel supply to the combustion chamber of a liquid rocket engine by spray nozzles

Ageenko Y.I., Bubnova A.S.

(Rus)

Vol 21, No 2 (2022)

Creation of promising technologies for producing holes in parts of a high-frequency ion engine

Ryazantsev A.Y., Yukhnevich S.S., Shirokozhuhova A.A.

(Rus)

Vol 20, No 3 (2021)

Analysis of basic concepts of advanced engines for supersonic civil aircraft on the basis of foreign designers’ experience

Alendar A.D., Grunin A.N., Siluyanova M.V.

(Rus)

Vol 22, No 3 (2023)

Experimental method for evaluating the balance of high-speed small-sized internal combustion engines

Rekadze P.D., Sychugov S.Y., Melentiev V.S., Rodionov L.V.

(Rus)

Vol 22, No 3 (2023)

Features of design calculation of compressor spool flow path of a twin-shaft gas turbine engine core on the basis of 1D and 2D models of their working process

Matveev V.N., Goriachkin E.S., Popov G.M., Baturin O.V., Kudryashov I.A.

(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)

Vol 22, No 1 (2023)

Results of conjugate modeling and analysis of the thermal state of a high-pressure turbine blade

Matveev V.N., Melnikov S.A., Popov G.M., Zubanov V.M., Kudryashov I.A., Shcherban A.I.

(Rus)

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

Comparative evaluation of the effectiveness of the application of perspective types of electric propulsion thrusters in the small spacecraft

Kulkov V.M., Obukhov V.A., Yegorov Y.G., Belik A.A., Krainov A.M.

(Rus)

Vol 23, No 1 (2024)

Investigation of the influence of broadband mechanical disturbances on the quality of recording interference patterns of GTE-wheel oscillations using a digital speckle pattern interferometer

Ivchenko A.V., Safin A.I.

(Rus)

Vol 21, No 4 (2022)

Series of diagnostic indicators of gearbox teeth wear in aircraft gas turbine engines

Sundukov A.Y., Shakhmatov Y.V.

(Rus)

Vol 21, No 2 (2022)

Influence of pad geometry and method of oil supply on the thermal state of GTE rotor tilting-pad journal bearing

Parovay E.F.

(Rus)

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

Research of influence of the thermal stream from the mid-flight liquid rocket engine on parameters of operating liquid rocket engines of small draught in the conditions of perspective razgonnogo's propulsion system of the block

Ageenko Y.I., Galperin R.N., Ivashin Y.S., Nigodjuk V.E., Ryzhkov V.V., Sulinov A.V.

(Rus)

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

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

1 1.

(Rus)

Vol 23, No 1 (2024)

Verification of aero-engine numerical rotor models based on virtual static structural and modal tests

Shaposhnikov K.V., Degtyarev S.A., Leontiev M.K., Anisimov S.V.

(Rus)

Vol 21, No 4 (2022)

Methodology for thermal calculation of the heat exchanger for cooling the air at the intake of the aerospace plane engine compressor

Panchenko S.L., Gras’ko T.V.

(Rus)

Vol 21, No 2 (2022)

Standardization of diagnostic indicators of gearbox teeth wear in aircraft gas-turbine engines

Sunduckov A.Y., Shakhmatov Y.V.

(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 22, No 4 (2023)

JSC “ODK” experience in implementing digital twin technologies in the design of gas turbine engines

Vinogradov K.A., Nikulin A.S., Shmotin Y.N.

(Rus)

Vol 21, No 4 (2022)

Calculation of optimum transfers from high-elliptic orbits to geostationary orbits using a stationary plasma engine

Kvetkin A.A., Kolesov A.V.

(Rus)

Vol 11, No 2 (2012)

Assessing the efficiency of flights to high near-earth orbits using boosters with chemical and electro-rocket engines

Ishkov S.A., Fadeenkov P.V., Balakin V.L.

(Rus)

Vol 23, No 2 (2024)

Modelling width of the spectral component of a gas-turbine engine gearbox output shaft speed

Sundukov A.E., Shakhmatov E.V.

(Rus)

Vol 15, No 4 (2016)

Analysis of low-thrust liquid rocket engines with a methane air pump unit

Ivanov A.I., Kositsin I.P., Borisov V.A.

(Rus)

Vol 23, No 2 (2024)

Aircraft electric power plants

Kondryakov A.D., Leontiev M.K.

(Rus)

Vol 23, No 2 (2024)

Comparative results of computational and theoretical study of the annular nozzle with a flat central body

Kirshina A.A., Levikhin A.A., Kirshin A.Y.

(Rus)

Vol 22, No 2 (2023)

New methods for identifying diagnostic indicators of the technical condition of aircraft gas turbine engine reduction gearboxes

Sundukov A.Y., Shakhmatov Y.V.

(Rus)

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

Design procedure of fundamental parameters of the direct-flow detonation pulsing engine

Porshnev V.A.

(Rus)

Vol 20, No 3 (2021)

Development of a methodology for calculating the working process of a small-size two-stroke internal combustion engine

Biryuk V.V., Gorshkalev A.A., Zakharov M.O., Larin V.L.

(Rus)

Vol 12, No 3-2 (2013): Vestnik SSAU

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 20, No 3 (2021)

Introduction to the problem of calculating the parameters of the mixing chamber of an afterburning bypass engine

Karev O.D.

(Rus)

Vol 19, No 3 (2020)

Improving the efficiency of aviation turbofan engines by using an intercooler and a recuperative heat exchanger

Omar H., Kuz'michev V.S., Tkachenko A.Y.

(Rus)

Vol 18, No 3 (2019)

Gas dynamic calculation of detonation in constant-cross-section ducts

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

(Rus)

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

Aspects of the numerical method calculating thermogazodynamic lrest based on not perfect passing of workflows in the combustion chamber

Silyutin M.V., Shustov S.A.

(Rus)

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

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

Egorychev V.S.

(Rus)

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

Testing of combined air-rocket engine mak-up with pulsing combustion chamber

Solodovnikov A.V., Vishegorodcev E.N., Golubyatnik V.V.

(Rus)

Vol 18, No 1 (2019)

Development of blend composition of aviation kerosene surrogate for the simulation of workflow of gas turbine engine combustion chamber

Matveev S.G.

(Rus)

Vol 17, No 4 (2018)

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.

(Rus)

Vol 17, No 3 (2018)

Evaluation of turbine rotor blade life taking into account static and thermal cyclic loading

Badamshin I.K.

(Rus)

Vol 16, No 3 (2017)

Selecting a squeeze film damper model for solving problems of gas turbine engine rotor dynamics

Leontiev M.K., Kutakov M.N.

(Rus)

Vol 15, No 4 (2016)

Unstady heat-mass-transfer and fuel distributions in flows downstream the gas-dynamic flame holder

Tretyakov V.V., Sviridenkov A.A.

(Rus)

Vol 15, No 2 (2016)

Empirical metod of predicting aviation piston engine noise

Moshkov P.A.

(Rus)

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

Research of hydrodynamic processes in the lubrication system of gas turbine engines

Gulienko A.I., Shchurovskiy Y.M.

(Rus)

Vol 14, No 1 (2015)

Possibility of using a bi-directional impulse turbine in a thermo-acoustic engine

Dovgjallo A.I., Shimanov A.A.

(Rus)

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

Development of thruster chamber operating on oxygen-hydrogen fuel

Salich V.L.

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

CFD-modeling of processes in a high-pressure oxidizer pump for the turbopump assembly of a liquid rocket engine

Zubanov V.M., Shabliy L.S.

(Rus)

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

Oxygen-hidrogen liquid rocket engine using turbo-pump developed for aviation hidrogen liquid two-spool turbo-jet

Ivanov A.I., Borisov V.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 11, No 2 (2012)

Numerical simulation of gas temperature spatial distribution in a full-size gas turbine combustor and its one-burner sector

Kostyuk V.Y., Kirilash Y.I., Stasyuk A.V., Shein V.V., Karzov D.V.

(Rus)

Vol 12, No 3-2 (2013): Vestnik SSAU

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)

Vol 10, No 3-1 (2011): Special Issue

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)

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

Experimental development of the LRE with CCCM nozzle’s extension

(Rus)

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

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)

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

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)

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

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)

Vol 12, No 3-2 (2013): Vestnik SSAU

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)

Vol 10, No 3-1 (2011): Special Issue

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)

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)

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

Мethod of design calculation of centrifugal emulsive duplex fuel nozzle

1 1.

(Rus)

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

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)

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

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)

1 - 100 of 269 Items 1 2 3 > >>

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