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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)

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)

1 1., 1 1.

(Rus)

Theoretical calculation approach of gas turbine engines compressor characteristic line

1 1.

(Rus)

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)

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)

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)

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

Barsukov O.A., Strizhenko P.P.

(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)

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 3-3 (2012): Special Issue

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

Rybakov V.N.

(Rus)

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

The use of electric engine to reduce the microaccelerations level of space lab

Sedelnikov A.V., Sygurova E.Y., Kireeva A.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

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

Results of primary operation of NK-37 engine low emission combustion system

Bantikov D.Y., Yeliseev Y.S., Lavrov V.N., Pchelyakov A.A., Fedorchenko D.G., Tsybizov Y.I.

(Rus)

Generation of control programes for disposable unmanned aircraft vehicle propulsion system by means of dynamic characteristic

Mikhailov A.Y., Akhmedzyanov D.A., Akhmetov Y.M., Mikhailova A.B.

(Rus)

Vol 10, No 1 (2011)

Kinematic and dynamic analysis of the basic mechanism of the Wankel engine, based on its vector model

Kosenok B.B.

(Rus)

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)

The simplification of heat engines thermodynamics calculation with using of idaeal gas’ model

1 1., 1 1.

(Rus)

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

Features of the new gas turbine aviation engines theory course

Mingazov B.G., Kosterin V.A., Varsegov V.L.

(Rus)

Vol 8, No 1 (2009)

Experimental analysis of flow separation in low thrust rocket engine nozzles with a profiled supersonic part of the nozzle

Shustov S.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 21, No 3 (2022)

Analysis of the influence of lubricant supply conditions on the pressure distribution in squeeze-film dampers

Novikov D.K., Shliandina N.S.

(Rus)

Vol 20, No 4 (2021)

Special aspects of numerical simulation of a two-stage axial-flow compressor with defective blades

Blinov V.L., Zubkov I.S., Iskortsev E.Y., Belyaev O.V., Plishkin P.I.

(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 3-4 (2011): Special Issue

Technique of conclusion the direct-flow detonation pulsing engine design to the leader position

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

(Rus)

Research of the possibility of thermal conditions LREST using an infrared thermal imaging system

Ryzhkov V.V., Silyutin M.V.

(Rus)

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

The possibilities of engine volumetric efficiency increasing at the expense of self-closing inlet valve

Kozin A.M., Rusakoff M.M.

(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)

Experimental research on the development of an “oxygen (gas) + kerosene” – fueled thruster

Salich V.L.

(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 17, No 1 (2018)

Methods of evaluating low-cycle fatigue of gas turbine engine parts exemplified by a high-pressure turbine cover plate

Kocherova E.E.

(Rus)

Vol 16, No 1 (2017)

Evaluation of low cycle fatigue based on the use of Coffin-Manson dependence under zero-to-“soft” loading cycle

Pavlov V.F., Kirpichyov V.A., Kocherova E.E., Zlobin A.S.

(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 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 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

Calculation of exciting aerodynamic load on a gas turbine engine compressor blade induced by the effect of a non-uniform gas flow

Ermakov A.I., Shklovets A.O., Fedorchenko D.G.

(Rus)

Computer-aided system of virtual gas turbine engine testing

Tkachenko A.Y., Rybakov V.N., Krupenich I.N., Ostapuk Y.A., Filinov E.P.

(Rus)

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

Rotary isochoric combustion chamber of a gas turbine engine

Porshnev V.A.

(Rus)

Vol 13, No 4 (2014)

Check and prediction of gas-turbine engine’s technical state

Zotin N.A.

(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

Problem formulation of bypass engine parameters optimization with a preselected gas generator

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

(Rus)

Hanges in volume combustion and concentration of nitrogen oxides in the exhaust gases gasoline engine

Kolomiets P.V.

(Rus)

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 1 (2011)

Definition of directions of developing methods, technical decisions and means of decreasing the technogenic influence on the environment for the omplementation on board of space launch vehicles

Shatrov Y.T., Baranov D.A., Trushlyakov V.I., Kudentsov V.Y.

(Rus)

Noise reduction of snow-plough

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

(Rus)

The story of invention and development of supercharge units of internal combustion engines

1 1., 1 1., 1 1.

(Rus)

Consideration of active forces at internal-combustion engine analysis in MSC.ADAMS environment

1 1., 1 1., 1 1.

(Rus)

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

Research of a seal work as an element of the air engine support

Vinogradov A.S., Rempel A.P.

(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 12, No 4 (2013)

Spacecraft preset orbital parameters control by means of thrusters

Salmin V.V., Volotsuev V.V., Shikhanov S.V.

(Rus)

Vol 21, No 3 (2022)

Gas-dynamic losses in the flow part of the channel charge of a solid-propellant rocket engine

A. N. Sabirzyanov A.N., Khamatnurova C.B., Kuzmin V.V.

(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)

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)

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)

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)

Estimating the efficiency of a bypass turbojet engine on the basis of a serial gas generator as a part of the power plant of a high-altitude unmanned aerial vehicle

Zinenkov Y.V., Lukovnikov A.V., Popov A.V., Nechaev V.N.

(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 16, No 1 (2017)

Improvement of gas turbine engines due to isothermal expansion in the turbine

Muraeva M.A., Gorjunov I.M.

(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 3-2 (2015): Special Issue

Conversion of gas turbine engine oil system

Boev A.A., Grishanov O.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 5-4 (2014): Special Issue

Iodine as an alternative propellant for electrojet engines

Ostrovskiy V.G., Smolentsev A.A., Scherbina P.A.

(Rus)