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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 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)

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)

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 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)

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 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 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 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 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 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)

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 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 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 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)

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 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 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 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)

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 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)

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)

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)

Fulfilment of initial design level of gas turbine engine using the methods of «ASTRA» CAE system

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

(Rus)

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

Development liquid roket engine on component fuel liquefied natural gas and oxygen for reusable space launching systems

Efimochkin A.F., Khrisanfov S.P., Golubyatnik V.V., Kafarena P.V., Yeliseyev 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)

Forecasting the individual performance capabilities of the rocket engine powerplant units at the maintanance stage

Biryuk V.V., Bronshtein V.M., Presnyakova A.S., Shatilova M.Y., Dostovalova S.S.

(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 13, No 1 (2014)

Development of a small-sized acoustic probe for the measurement of pressure pulsations in the gasdynamic duct of gas turbine engines

Gimadiyev A.G., Bystrov N.D., Ilyinsky S.A.

(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 9, No 1 (2010)

Dynamic analysis and optimization of turbojet engine nozzle control mechanism

(Rus)

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

Development of advanced low thrust rocket engines with ecologically friendly propellants

1 1., 1 1., 1 1.

(Rus)

Vol 8, No 3-2 (2009): Special Issue

Features of calculation of hydraulic characteristics of capillary spray jets of is liquid-stnyh rocket engines of small pull-rod

1 1., 1 1., 1 1.

(Rus)

Vol 8, No 3-2 (2009): Special Issue

Operate reliability enhancement of thermogenerator modules for heat engine with acoustic emission method

1 1.

(Rus)

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

Wearability, wearproof and heat-shielding coverings for details of the gas path of the turbine, the compressor and the chamber of combustion of gas turbine engine

Barvinok V.A., Shitarev I.L., Bogdanovich V.I., Dokukina I.A., Karasev V.M.

(Rus)

Vol 7, No 1 (2008)

Identification of a gas turbine engine mathematical model by the ressults of testing

Botchkaryov S.K., Dmitriyev A.Y.

(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)

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)

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 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)

The determination of the thermoacoustic generator aspect from electrodynamic unit features by the parametric-studies

Vorotnikov G.V., Kruchkov A.N., Zynovyev E.A.

(Rus)

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

Physical workflow model in the combustion chamber LREST with a jet-centrifugal jets on hypergolic propellants

Silyutin M.V., Shustov S.A.

(Rus)

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

Calculation of indicator diagram dynamic test at internalcombustion engine in KDAM environment

Kosenok B.B.

(Rus)

Vol 17, No 4 (2018)

Optimization of fuel distribution in the afterburner of a gas turbine engine

Nelyubin V.R.

(Rus)

Vol 17, No 3 (2018)

Evaluation of turbine rotor blade life taking into account static and thermal cyclic loading

Badamshin I.K.

(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 15, No 1 (2016)

System-mathematical simulation of engine air hydraulic power supply

Goryunova N.R., Goryunov A.A.

(Rus)

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

Application of numerical simulation systems for the research of the blade casting process in blank production

Smelov V.G., Vdovin R.A., Agapovichev A.V.

(Rus)

Vol 10, No 5 (2011)

Simulation of aerodynamic structure of the flow in the combustion chamber of a small-size gas turbine engine with the help of CAE–systems

Matveev S.G., Orlov M.Y., Abrashkin V.Y., Zubrilin I.A., Matveev S.S.

(Rus)

Vol 14, No 2 (2015)

Strength analysis of internal combustion engine elements by using ANSYS with taking into account heat processes in the combustion chamber

Biryuk V.V., Gorshkalev A.A., Kayukov S.S., Saigakov E.A.

(Rus)

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

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 5-1 (2014): Special Issue

Conception of cycle life additivity and its application for determining the resource of aero engine disks

Tumanov N.V., Lavrentyeva M.A.

(Rus)

Seal designing as element of aircraft engine systems and engine units

Vinogradov A.S.

(Rus)

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

Development of a virtual prototype of gasturbine engine at the stage of conceptual thermogasdynamic designusing the CAE-system «ASTRA»

Tkachenko A.Y., Krupenich I.N.

(Rus)

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

Robust research of the fuzzy logic controllers using a fuel flow control loop of the gas-turbine engine as an example

Chicherova E.V.

(Rus)

Vol 11, No 2 (2012)

Joint works of Ilyushin design bureau and general designer N. D. Kuznetsov

Novozhilov G.V.

(Rus)

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

Methods and means of aircraft gas turbine engine conceptual design underlying the CAE system «ASTRA»

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

(Rus)