Search

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

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 2 (2013)

Flame propagation velocity and ionization in burning gasoline and methane with addition of hydrogen

Shaykin A.P., Ivashin P.V., Galiev I.R.

(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)

Internal combustion engine some cooling system components detailed calculation

Kolomin I.V., Ajukov A.A., Birjuk V.V.

(Rus)

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

Methodology of optimization of parameter of matching the combustion chamber and turbine joint operation

Grigoriev A.V., Golubchikov P.P., Ilushin M.Y., Rudakov O.A., Solovieva A.V.

(Rus)

Vol 18, No 1 (2019)

Development of blend composition of aviation kerosene surrogate for the simulation of workflow of gas turbine engine combustion chamber

Matveev S.G.

(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)

Micro gas turbine engine imitation model

Kuznetsov A.V., Makaryants G.M.

(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 4 (2015)

Relationship between carbon concentration in a fuel and characteristics of flame propagation with a magnitude of ion current

Shaykin A.P., Budaev S.I., Galiev I.R.

(Rus)

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

Research of hydrodynamic processes in the lubrication system of gas turbine engines

Gulienko A.I., Shchurovskiy Y.M.

(Rus)

Vol 10, No 5 (2011)

Functional analysis of periodic disturbances during intermittent cutting

Kolodyazhny D.Y.

(Rus)

Vol 14, No 1 (2015)

Computer-aided design of aircraft gas turbine engines and selection of materials for their main parts

Akhmedzyanov D.A., Kishalov A.E., Markina K.V.

(Rus)

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

Verification of energy efficiency of a low-thrust liquid-propellant engine with the deflector-centrifugal injecting pattern

Ageenko Y.I., Pegin I.V.

(Rus)

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

The influence of the shuttle effect on the intensification of heat losses in a Stirling engine

Savchenko V.A., Stolyarov S.P.

(Rus)

Vol 11, No 7 (2012)

Building foundations of virtual information-based educational environment

Zelenko L.S., Zagumennov D.A., Zinchenko A.O.

(Rus)

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

A simplified method of thermoacoustic engine analysis

Zynovyev E.A., Dovgyallo A.I.

(Rus)

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

Investigation of the possibility of the creation LREST by thrust 400 N with a baffle - centrifugal scheme of NT and NDMG mixing

Ageenko Y.I., Ilin I.V., Pegin I.V., Shalamov E.A.

(Rus)

Vol 11, No 2 (2012)

Numerical simulation of gas temperature spatial distribution in a full-size gas turbine combustor and its one-burner sector

Kostyuk V.Y., Kirilash Y.I., Stasyuk A.V., Shein V.V., Karzov D.V.

(Rus)

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

Evaluation of internal combustion engine cycle work using an ionic current sensor

Ivashin P.V., Ramazanov M.P., Tverdokhlebov A.Y., Shaikin A.P., Yasnikov I.S.

(Rus)

Operational testing of thermoplastic reinforced blades

Krutsilo V.G., Krotinov N.B.

(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 2 (2011)

Construction of a blade beam finite element as a component of the blade disk rotary-symmetrical system

Davydov D.P.

(Rus)

Vol 10, No 1 (2011)

Optimal program of controlling continuous low thrust in the flight between noncoplanar elliptical and geostationary orbits

Fadeenkov P.V., Ishkov S.A.

(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)

Oxyhydrogen propulsion device base on water electrolysis and lrest on component H2 + O2 for control system SS

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

Simulation of the distributed selection and supply of cooling air in gas-turb engine

Goryunov A.I., Goryunov I.M.

(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 2 (2013)

Investigation of energy parameters of small-thrust liquid rocket engines with the geometric expansion ratio of the nozzle F=200

Ageenko Y.I., Nigodyuk V.E., Ryzhkov V.V., Sulinov A.V., Shustov S.A.

(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)

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

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)

Aircraft engine design based on unified gas generator

Vinogradov A.S., Parovay Y.F., Mordvinov A.G., Popov D.V., Shirokov M.A.

(Rus)

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

On selection of automatic control system for crvogenic fuel gas turbine engine

Bukin V.A.

(Rus)

Vol 18, No 1 (2019)

Influence of the stressed state of the surface layer on the endurance of gas turbine engine compressor blades

Sazonov M.B., Solovatskaya L.V.

(Rus)

Vol 17, No 4 (2018)

Theory and calculation of parameters of the detonation engine thermodynamical cycle

Grigoriev A.V., Mitrofanov V.A., Rudakov O.A., Solovieva A.V.

(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)

Some issues of research and development in aviation industry

Korchak V.Y., Kuznetsov V.V., Borisenkov I.L., Leonovich G.I., Lukachev S.V., Biryuk V.V.

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

Dynamic behaviour of high- bypass- ratio turbofan carbon fiber-reinforced plastic blade ubder unsteady airloads

Buyukli T.V., Fedorchenko Y.P., Shorstov V.A.

(Rus)

Vol 10, No 5 (2011)

Increasing the capacity of engine intake system

Kozin A.M., Rusakov M.M.

(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 5-1 (2014): Special Issue

CFD-modeling of processes in a high-pressure oxidizer pump for the turbopump assembly of a liquid rocket engine

Zubanov V.M., Shabliy L.S.

(Rus)

Vol 11, No 5-2 (2012): Special Issue

Analysis of the cause of serious flight accident

Vakhrushev D.E., Agaphonov O.A., Pryadko S.P., Schukin A.V.

(Rus)

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

The modeling of the thermoacoustic electric generator by quadrupole approximation approach

Vorotnikov G.V.

(Rus)

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

Problem of multistage compressor optimization while designing perspective gas turbine engines

Shabliy L.S.

(Rus)

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

About some directions in development avation engine buildings

Zamtfort B.S.

(Rus)

Vol 11, No 2 (2012)

Numerical simulation of gas temperature spatial distribution in a one-burner sector of a gas turbine combustor with uncertain initial conditions of fuel atomization

Kostyuk V.Y., Kirilash Y.I., Stasyuk A.V., Shein V.V., Karzov D.V.

(Rus)

The projecting of gas turbine engine composite blades

Ryzhov A.A., Galimkhanov B.K., Ryzhov N.A., Latypov R.K., Irgalin S.R.

(Rus)

Guaranteeing of ecological and economic indicators of internal combustion engine

Grabovskiy A.A., Mironov V.A.

(Rus)

Vol 10, No 2 (2011)

Construction of a promising face gas-dynamic seal of the aircraft engine

Bondarchuk P.V., Falaleev S.V.

(Rus)

Vol 9, No 4 (2010)

Parametric analysis of thermoacoustic travelling-wave engine operation with external heat application

Dovgyallo A.I., Zynovyev Y.A., Vorotnikov G.V.

(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 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

Characteristics of the sampling instrument for measuring emissions of an aircraft gas turbine engine

Okhlobystin A.V., Lyubimov R.V., Sokolova N.N.

(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)

Design of experiments for verification of computational life prediction methods

Samsonova O.V., Fetisov K.V., Karpman I.V., Burtseva I.V.

(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)

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)

Influence of the geometry fidelity of resonant sound-absorbing liner samples on their acoustic characteristics

Kustov O.Y., Khramtsov I.V., Bulbovich R.V.

(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 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)

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

Muraeva M.A., Gorjunov I.M.

(Rus)

Vol 15, No 3 (2016)

The influence of booster design features on aicraft engine fan tonal noise

Khaletskiy Y.D., Korzhnev V.N., Pochkin Y.S.

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

Modification of the starter turbine disk for blade containment certification tests

Karimbaev K.D., Sapronov D.V.

(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 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)

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

Development of a single-section demonstrator rotary engine on the basis of a modern complex design procedure

Kostyuchenkov A.N., Zelentsov A.A., Semenov P.V., Minin V.P.

(Rus)

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

Research of the influence of design parameters of a 400 N-thrust low-thrust liquid rocket engine on its energy efficiency

Ageenko Y.I., Ilyin R.V., Pegin I.V.

(Rus)

Vol 11, No 5-2 (2012): Special Issue

Thermoplastic strengsening of blades aircraft gas turbine engines

Krotinov N.B.

(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

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)

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)

, ,

(Rus)