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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)

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)

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)

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

Approaches to parametric models of blade machines formation

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

(Rus)

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

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)

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

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)

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)

Development of advanced low thrust rocket engines with ecologically friendly propellants

1 1., 1 1., 1 1.

(Rus)

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)

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)

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

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)

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

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)

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)

Definition of overall limits internal-combustion engine using vector modeling

Kosenok B.B.

(Rus)

Vol 13, No 1 (2014)

Analysis of nonstationary thermal state of a low-thrust liquid rocket engine taking into account injection, evaporation and combustion of liquid fuel droplets

Vorobiev A.G., Borovik I.N., Ha S.

(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 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)

Manipulate pulsed detonation engine

1 1., 1 1.

(Rus)

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

Improvement of a design piston of diesel engine of tractor

Rogdestvensky Y.V., Doykin A.A., Murzin V.S.

(Rus)

Vol 8, No 2 (2009)

Dependence of the extent to which the space vehicle’s own atmosphere and plasma generated by stationary plasma engines affect the space vehicle on its structural lay-out

Testoyedov N.A., Smirnov V.A.

(Rus)

Vol 12, No 1 (2013)

Optimal control of the angle of attack of a hypersonic flight vehicle

Bebyakov A.A.

(Rus)

Vol 12, No 4 (2013)

The usage of high power supply capacity transport spacecraft

Ivanovich S.N.

(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)

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

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

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

Egorychev V.S.

(Rus)

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

The numerical modelling of processes in combustion chambers of low thrust rocket engines

Salich V.L.

(Rus)

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

Repair of aircraft engine and respective conception under the condition of modern production at manufacturing plants and engine operability recovery centers

Steshenko I.G., Panov V.A.

(Rus)

Vol 17, No 4 (2018)

Proposals for improving the efficiency and service life of the turbines of turbo-pump assemblies in liquid-propellant rocket engines by using double-sided crest-type radial labyrinth seals

Levochkin P.S., Chvanov V.K., Vasiliev V.S., Timushev S.F.

(Rus)

Vol 17, No 3 (2018)

Refining methods of vibration diagnostics of wear of turbo-prop engine differential speed reduction unit gear teeth

Avramenko A.A., Kryuchkov A.N., Plotnikov S.M., Sundukov E.V., Sundukov A.E.

(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 10, No 6 (2011)

Estimation of the required thrust impulse for small spacecraft (SSC) control system with a propulsion system using fuel gas components

Titov B.A., Koltsov I.V.

(Rus)

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

Procedure of validated CFD-modeling of a two-stage screw-centrifugal pump

Zubanov V.M., Shabliy L.S., Krivtsov A.V., Ivanov A.I., Kositsin I.P., Baturin N.V.

(Rus)

Vol 10, No 5 (2011)

Modeling of propane combustion processes in case of converting a GTE combustion chamber to gaseous fuel

Matveev S.G., Lanskiy A.M., Orlov M.Y., Abrashkin V.Y., Dmitriev D.N., Zubrilin I.A., Semenov A.V.

(Rus)

Vol 14, No 1 (2015)

Vortex cleaning of fuel tank pressurant gas

Biryuk V.V., Shimanov A.A., Onoprienko D.A., Smorodin A.V., Shepelev A.I.

(Rus)

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

Numerical simulation of tonal noise of a bypass engine fan stage

Pyatunin K.R., Arharova N.V., Remizov A.E.

(Rus)

Vol 13, No 5-1 (2014): Special Issue

Design of the gas turbine engine rotor wheel with ceramic blades

Sapronov D.V., Reznik S.V.

(Rus)

Vol 13, No 4 (2014)

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

Zotin N.A.

(Rus)

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

Design solutions to provide thermal protection of three-shaft turbofan engine turbine support oil cavities

Petrukhin A.G., Boev A.A., Butylkin S.V.

(Rus)

Vol 11, No 2 (2012)

Some peculiarities of high-altitude starting of engines of the RD-33 type

Kotsyubinsky S.V., Ravikovich Y.A.

(Rus)

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

Kolomiets P.V.

(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 13, No 1 (2014)

Analysis of nonstationary thermal state of low-thrust liquid rocket engine with high-concentration hydrogen peroxide and kerosene propellant with film cooling

Vorobiev A.G., Borovik I.N., Ha S.

(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)

Vol 9, No 1 (2010)

Influence of the loading parameter on the efficiency ofa three-stage turbine of turbojet bypass engine

1 1., 1 1.

(Rus)