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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 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 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 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 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 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 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 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 23, No 2 (2024)

The relevance of introducing a requirements management system in the production process of the aircraft engine construction industry

Malinovskiy I.M., Starodumov A.V., Myagkov K.A., Yusipov B.K.

(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 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 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 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 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 23, No 2 (2024)

Aircraft electric power plants

Kondryakov A.D., Leontiev M.K.

(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 21, No 3 (2022)

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

Sunduckov A.E.

(Rus)

Vol 21, No 1 (2022)

Gasdynamic and strength improvement of the axial flow turbine of a helicopter gas turbine engine

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

(Rus)

Vol 19, No 1 (2020)

Bringing spacecraft into solar-oriented attitude by the measurements of a single-axis angular-rate sensor and an optical solar sensor

Shipov M.G., Steklova A.A., Davydov A.A.

(Rus)

Vol 18, No 3 (2019)

Mathematical model for calculating the mass of a heat exchanger in problems of optimizing the parameters of the working process of aircraft gas turbine engines

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

(Rus)

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

Influence in a constructive and regime parameters antechamber by operation-in the combustion chamber liquid-propellant rocket engine thrusters on hypergolic liquid propellants

Nigodjuk V.E., Sulinov A.V.

(Rus)

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

Sales training methods based on through the use of CAD / CAM / CAE systems for aero engines

Balyakin A.V., Ermakov A.I., Pronichev N.D., Chempinsky L.A.

(Rus)

Vol 18, No 2 (2019)

Research of hafnium-containing defects in granular nickel EP741NP alloy using electron microscopy

Trunkin I.N., Artamonov M.A., Ovcharov A.V., Vasiliev A.L.

(Rus)

Vol 17, No 4 (2018)

Numerical simulation of low liquid flow in a mixer consisting of two centrifugal swirlers

Semkin E.V.

(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 16, No 3 (2017)

Locally optimal control of space tug motion between the libration points of the Earth-Moon system

Starinova O.L., Fain M.K.

(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 3-2 (2015): Special Issue

Conversion of gas turbine engine oil system

Boev A.A., Grishanov O.A.

(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 14, No 2 (2015)

Vibrodiagnostics of turboprop engine gearbox wear

Sundukov A.Y., Sundukov Y.V., Plotnikov S.M.

(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

Automated thermovacuum firing test facility for testing and research of workflow in low-thrust rocket engine on hypergolic propellants

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

(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 4 (2012)

Modeling oil separation in the impeller of a radial-type centrifugal breather

Petrukhin A.G., Tryanov A.E.

(Rus)

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

Optimization features of the working process parameters of bypass engine on the basis of given gas generator

Rybakov V.N.

(Rus)

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

Influence of high technologies on production technological prototypes of missile engines

Kodencev S.N., Suhochev G.A.

(Rus)

Vol 11, No 2 (2012)

Mathematical model and peculiarities of operating mobile robots with hybrid drives

Ilyukhin Y.V., Tatarintseva A.V.

(Rus)

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

Influence of the initial design data uncertainty on the choice of optimal working process parameters of gas turbine engine

Kuzmichev V.S., Tkachenko A.Y., Rybakov V.N., Krupenich I.N., Kulagin V.V.

(Rus)

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

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)

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

Studying the influence of the gas-dynamic non-stationary factors on the mathematical modelling of the gas turbine engines nonsetup work modes

Kofman V.M.

(Rus)

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

Methodical features of vibration tests of rotating blades using dynamic spin rigs

Nozhnitsky Y.A., Fedina Y.A., Shadrin D.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)

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

Experimental development of the LRE with CCCM nozzle’s extension

(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 3-2 (2009): Special Issue

Increasing efficiency of pressurization of the rocket tanks in the flight

1 1., 1 1.

(Rus)

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

Project of 30 000 h.p. power gas turbine

Zrelov V.A.

(Rus)

Vol 7, No 3 (2008): Special Issue

Increasing efficiency of pressurization of the rocket tanks in the flight

Biryuk V.V., Kapitonov V.A., Smorodin A.V.

(Rus)

Vol 21, No 3 (2022)

Aspects of simulating stable low-cycle fatigue crack growth in the main parts of aircraft gas turbine engines

Ryabov A.A., Mokhov K.Y., Voronkov O.V., Kudryavtsev A.Y., Museev A.A.

(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 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 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 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

Increasing the energy efficiency of liquid rocket engine of small thrust (0,1-1,0) N with jet scheme of mixing

Nigodjuk V.E., Sulinov A.V.

(Rus)

Vol 18, No 2 (2019)

Calculation of lubricant flow in the slide bearing of the aviation engine reducer

Siluyanova M.V., Fertikov A.О.

(Rus)

Vol 17, No 4 (2018)

Impact of the turbulence modeling approach on the accuracy of the fan noise level prediction

Pyatunin K.R., Arkharova N.V.

(Rus)

Vol 17, No 3 (2018)

Analysis of schemes of correction of dynamic characteristics of acoustic probes for measuring pressure pulsations in a gas turbine engine

Gimadiev A.G., Bystrov N.D., Dyagileva E.S.

(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)

Peculiarities of the working process of low-thrust hypergolic-propellant liquid rocket engines with a thrust of less than 1 N

Nigodjuk V.E., Sulinov A.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 3-2 (2015): Special Issue

Procedure of creating three-dimensional solid models of tool electrodes for electrochemical pulse machining of gas turbine engine parts in CAD-systems with their parametric coupling with software module profiling

Nekhoroshev M.V., Pronichev N.D., Smirnov G.V.

(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 2 (2015)

Identifying the causes of excessive vibration in gas turbine engines in the course of their rig tests

Sundukov A.Y., Sundukov Y.V., Plotnikov S.M.

(Rus)

1 - 100 of 304 Items 1 2 3 4 > >>

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