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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)

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)

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

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)

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

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

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

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)

201 - 269 of 269 Items << < 1 2 3

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