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Vol 22, No 1 (2023)

The problems of creating a propulsion system of a new generation supersonic passenger aircraft (review)

Alendar A.D., Lanshin A.I., Evstigneev A.A., Yakubovsky K.Y., Siluyanova M.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 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 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)

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

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

Shishkov V.A.

(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 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 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)

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 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 10, No 6 (2011)

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

Shishkov V.A.

(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 3-3 (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 23, No 1 (2024)

Optimization of trajectory motion of the first stage of an aerospace system

Khramov A.A.

(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 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)

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 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 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 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 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)

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

Seal designing in a structure of the cooling system in gas turbine engine

Vinogradov A.S., Myatlev A.S.

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

Test bench for investigation of thrusters intra-chamber working processes

Pervyshin A.N., Ryazanov A.I.

(Rus)

Vol 15, No 2 (2016)

Empirical metod of predicting aviation piston engine noise

Moshkov P.A.

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

Estimation of parameters of a pulse detonation engine (РDЕ)

Anakin A.T., Tsybizov Y.I.

(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 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)

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)

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 22, No 2 (2023)

Influence of complex loading of radial bearings of the oscillation groups of liquid propellant engine steering gear on the frictional moment

Balyakin V.B., Lavrin A.V., Dolgikh D.E.

(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 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 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 3 (2022)

Determination of the optimal parameters and engine layout for a strike unmanned aerial vehicle

Zinenkov Y.V., Lukovnikov A.V., Agaverdyev S.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)

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 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 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)

Application of the vacuum casting technology in the production of small-size gas turbine engine blade machines

Faramazyan A.M., Remchukov S.S., Demidyuk I.V.

(Rus)

Vol 19, No 4 (2020)

The effect of heat recovery on the optimal values of helicopter turboshaft engine parameters

Omar H.H., Kuz'michev V.S., Zagrebelnyi A.O., Grigoriev V.A.

(Rus)

Vol 18, No 4 (2019)

Verification of a design model and evaluation of a technique of manufacturing aircraft engine composite parts on the basis of dynamic tests

Zinin A.V., Arkhipov A.N., Kholobtsev D.P., Ravikovich Y.A., Shevjakov A.O., Kholmanova M.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

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.

(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 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)

Micro gas turbine engine imitation model

Kuznetsov A.V., Makaryants G.M.

(Rus)

Vol 15, No 4 (2016)

Method of transient simulation of combustion processes in a low-thrust rocket engine operating on gaseous hydrogen and oxygen

Zubanov V.M., Shabliy L.S., Stepanov D.V.

(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 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 10, No 5 (2011)

Functional analysis of periodic disturbances during intermittent cutting

Kolodyazhny D.Y.

(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 5-3 (2014): Special Issue

Verification of energy efficiency of a low-thrust liquid-propellant engine with the deflector-centrifugal injecting pattern

Ageenko Y.I., Pegin I.V.

(Rus)

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

The influence of the shuttle effect on the intensification of heat losses in a Stirling engine

Savchenko V.A., Stolyarov S.P.

(Rus)

Vol 11, No 7 (2012)

Building foundations of virtual information-based educational environment

Zelenko L.S., Zagumennov D.A., Zinchenko A.O.

(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 3-1 (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 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

Evaluation of internal combustion engine cycle work using an ionic current sensor

Ivashin P.V., Ramazanov M.P., Tverdokhlebov A.Y., Shaikin A.P., Yasnikov I.S.

(Rus)

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

Operational testing of thermoplastic reinforced blades

Krutsilo V.G., Krotinov N.B.

(Rus)

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

Progressive thermodynamic cycle of internal combustion engine based on сrank a rod the mechanism with dual kinematic communications

Grabovskiy A.A.

(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 10, No 1 (2011)

Optimal program of controlling continuous low thrust in the flight between noncoplanar elliptical and geostationary orbits

Fadeenkov P.V., Ishkov S.A.

(Rus)

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

Motion trajectories of the vehicle with mass injection pre-compressor cooling turbojet engines as the first stage of aircraft-space systems

1 1., 1 1.

(Rus)

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

Oxyhydrogen propulsion device base on water electrolysis and lrest on component H2 + O2 for control system SS

1 1., 1 1., 1 1., 1 1., 1 1.

(Rus)

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

The interconnection between the benzo(a)pyrene and the soot emissions heat-engine using hydrocarbons fuels

1 1., 1 1., 1 1., 1 1.

(Rus)

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

Simulation of the distributed selection and supply of cooling air in gas-turb engine

Goryunov A.I., Goryunov I.M.

(Rus)

Vol 8, No 1 (2009)

Identification and procedure of reducing periodic noise of internal combustion car engines using the active compensation method

Vasilyev A.V., Andreyev S.S., Butsayev I.V., Pimkin V.V.

(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 19, No 4 (2020)

Investigation of the characteristics of the component of vibration of gas turbine engine gearbox that causes fatigue failures of its structural elements in case of tooth flank wear

Sundukov A.E.

(Rus)

Vol 18, No 3 (2019)

Design of experiments for verification of computational life prediction methods

Samsonova O.V., Fetisov K.V., Karpman I.V., Burtseva I.V.

(Rus)

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

Gas turbine engine rotor bearings electrical current damage on the base of NK-family engines for electrical generator drive

Nazdrachev S.V.

(Rus)

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

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)

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 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)

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 1 (2018)

Optimization of ducted counter–rotating fan blades on the basis of solving a 3d inverse problem with the aim of improving fan gasdynamic characteristics

Mileshin V.I., Pankov S.V., Fateyev V.A., Shchipin S.K.

(Rus)

Vol 16, No 2 (2017)

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.

(Rus)

Vol 15, No 4 (2016)

Using the «virtual engine» software in automatic control system of gas turbine engine

Golberg F.D., Gurevich O.S., Petukhov A.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 14, No 3-1 (2015): Special Issue

Dynamic behaviour of high- bypass- ratio turbofan carbon fiber-reinforced plastic blade ubder unsteady airloads

Buyukli T.V., Fedorchenko Y.P., Shorstov V.A.

(Rus)

Vol 10, No 5 (2011)

Increasing the capacity of engine intake system

Kozin A.M., Rusakov M.M.

(Rus)

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

Experience in the development of 11Д58MФ liquid rocket engines

Smolentsev A.A.

(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 5-2 (2012): Special Issue

Analysis of the cause of serious flight accident

Vakhrushev D.E., Agaphonov O.A., Pryadko S.P., Schukin A.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

Problem of multistage compressor optimization while designing perspective gas turbine engines

Shabliy L.S.

(Rus)

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

About some directions in development avation engine buildings

Zamtfort B.S.

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

The projecting of gas turbine engine composite blades

Ryzhov A.A., Galimkhanov B.K., Ryzhov N.A., Latypov R.K., Irgalin S.R.

(Rus)

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

Guaranteeing of ecological and economic indicators of internal combustion engine

Grabovskiy A.A., Mironov V.A.

(Rus)

Vol 10, No 2 (2011)

Construction of a promising face gas-dynamic seal of the aircraft engine

Bondarchuk P.V., Falaleev S.V.

(Rus)

1 - 100 of 297 Items 1 2 3 > >>

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