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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 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 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 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 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 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)

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)

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

Aerodynamic improvement of GTE compressors by space profiling of blade vanes

Gerasimenko V.P., Shelkovsky M.Y.

(Rus)

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

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)

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

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)

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

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)

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

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)

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

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)

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

1 1., 1 1.

(Rus)

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

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)

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

Working out the system of technical decisions for ensuring the reliability of friction units of gas-turbine engines

Gromakovsky D.G., Kovshov A.G., Ibatullin I.D.

(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 3-1 (2013): Vestnik SSAU

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 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)

Parametric study of the influence of location and extension height of the rod interceptor on jet engine nozzle characteristics

Tishchenko K.O., Brykov N.A., Belyaeva A.S.

(Rus)

Vol 19, No 4 (2020)

Сalculation of characteristics of atomization of liquid supplied at an angle to the flow direction and justification of adjusting the angle of the nozzle inclination relative to the gas flow

Teslya D.N., Mityaev S.V., Drobyshev P.A.

(Rus)

Vol 18, No 4 (2019)

Improvement of fretting wear resistance of blade root made of polymer composite material

Karimbayev T.D., Afanasiev D.V., Matyukhin D.V., Orlov M.A.

(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

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

Egorychev V.S.

(Rus)

Vol 18, No 2 (2019)

Ensuring permissible level of gas turbine dynamic loading in operation by means of standard engine control devices

Chervonyuk V.V., Korovin B.B.

(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)

Engines for domestic drones: past, present and future

Cherkasov A.N., Legkonogikh D.S., Zinenkov Y.V., Panov S.Y.

(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)

Micro gas turbine engine imitation model

Kuznetsov A.V., Makaryants G.M.

(Rus)

Vol 14, No 3-2 (2015): Special Issue

Development and analysis of screw restrictor hydraulic characteristics in the air bleed valve control unit of a gas turbine engine

Gimadiev A.G., Makaryants G.M., Blyumin K.V., Dudnichenko I.M.

(Rus)

Vol 10, No 5 (2011)

Vortex gas wind-driven power plant for supplying compressor stations with electrical energy

Biryuk V.V., Zubrilin I.A., Krasnorutskiy A.S.

(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 5-3 (2014): Special Issue

Results of hot tests of an oxygen preburner of a liquid-propellant engine 11D58MF

Barsukov O.A., Strizhenko P.P.

(Rus)

1 - 100 of 263 Items 1 2 3 > >>

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