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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

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

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 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)

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

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

(Rus)

Hard & soft complex for “Angara” family launch vehicles engine system development

Partola I.S.

(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 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

A separator skidding in the cylindrical roller bearing between shafts of the gas turbine engine

1 1., 1 1., 1 1.

(Rus)

Development and study of the designs of sprayers with increased speed for internal combustion engine (ice)

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(Rus)

Mixing parameters investigations and methods of approach to calculations and development of the thrusters with a spray-centrifugal scheme of NT and NDMH mixing on the confusion chamber wall in considered

1 1.

(Rus)

Vol 8, No 1 (2009)

Problems of making auxiliary gas turbine engines with gas bearing rotors

Ponomaryov B.A., Gavrilov V.V.

(Rus)

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

Development of an algorithm of design calculation of a combustion chamber for microturbine electric power plants

Matveev S.G., Abrashkin V.Y., Orlov M.Y., Lansky A.M., Makarov N.S., Matveev S.S., Anisimov M.Y.

(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 2 (2020)

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

Kuznetsov A.V., Makaryants G.M.

(Rus)

Vol 18, No 3 (2019)

Life of gas turbine engine components under corrosive exposure

Pivovarova M.V., Gladkiy I.L.

(Rus)

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

Working process of gaseous fuel metallizator

Pervyshin A.N., Ryazanov A.I.

(Rus)

To a question of forcing up of thermal stirlings macine

Belozertcev V.N.

(Rus)

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 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 3 (2018)

Engines for domestic drones: past, present and future

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

(Rus)

Vol 16, No 4 (2017)

Development of a new collector device for gas turbine engine afterburner

Teslya D.N., Mayatsky S.A., Grasko T.V.

(Rus)

Vol 15, No 4 (2016)

Application of structure-energy failure theory for determining the probability of failure and durability of turbine and compressor blades of aircraft engines

Chernyaev A.I., Trefilov V.A.

(Rus)

Vol 15, No 3 (2016)

Laser powder weld reconditioning of gas turbine engine blades

Korsmik R.S., Turichin G.A., Klimova-Korsmik O.G., Zemlyakov E.V., Babkin K.D.

(Rus)

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

Testing of gas turbine engine bearing oil supply through an oil-catch ring

Boev A.A., Petrukhin A.G., Mikhailov A.A.

(Rus)

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

Application of the cyclic life additivity concept for the determination of service life of aero engine disks made from powder alloys

Tumanov N.V., Lavrentyeva M.A., Vorobyeva N.A., Kalashnikova A.I.

(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

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 5-1 (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 5-2 (2012): Special Issue

Simulation design, kinematic and dynamic analysis of "virtual piston engine"

Gvozdev A.S., Melentjev V.S.

(Rus)

Gas turbine engine designing on the basis of a unified gas generator

Rybakov V.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 14, No 3 (2014)

Application of thermoplastic hardening for restoration of fatigue durability of gas turbine disks

Vishnyakov M.A.

(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

Aerodynamic improvement of GTE compressors by space profiling of blade vanes

Gerasimenko V.P., Shelkovsky M.Y.

(Rus)

Estimate of key parameters of a gas turbine engines with application of the modelling procedure of the equilibrium state of homogeneous mixture of hydrocarbon fuel combustion products

Boldyrev O.I., Gorynov I.M.

(Rus)

The combined fuel draining control system for liquid oxygen and liquid hydrogen upper stage

Ivanov V.P., Partola I.S.

(Rus)

Vol 10, No 1 (2011)

Analysis of economic and organizational problems in aircraft engine construction

Nikitin N.F., Cherner N.V.

(Rus)

Vol 9, No 2 (2010): Special Issue

Optimization methods of design-ballistic characteristics circumterraneous and interplanetary space vehicle with electrojet engines of low thrust

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

(Rus)

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

Experimental determination of the side forces acting on the combustion chamber in the altitude chamber at startup

, , , ,

(Rus)

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

1 1.

(Rus)

Probabilistic estimate of compressor blades durability to foreign object damage

1 1., 1 1.

(Rus)

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

The oretical substantiation of the constructive scheme of the air-gas tract rinsing device for GTE

Silaev B.M., Mal’tsev E.N.

(Rus)

Vol 7, No 3 (2008): Special Issue

The phase characteristic of force cutting and its role in occurrence and development of self-oscillations at sharpening not rigid details of aviation engines

Burmistrov E.V., Basyrov M.N., GiniyatuIIin R.R.

(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)

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)

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)

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)

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)

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)

Мethod of design calculation of centrifugal emulsive duplex fuel nozzle

1 1.

(Rus)

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)

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)

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

Automated profiling of tool electrode in electrochemical pulse machining

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

(Rus)

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

Multicriterial choice of the best variant of the pulse detonation engine design for aircraft angular stabilization and orientation systems

Safronov V.V., Porshnev V.A., Zhebrakov A.S.

(Rus)

Approaches to parametric models of blade machines formation

Shabliy L.S., Popov G.M., Kolmakova D.A.

(Rus)