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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 14, No 3 (2014)

Research of a heat-resistant intermetallic underlayer for the heat-shielding coating of gas turbine engine turbine blades

Tarasenko Y.P., Tsareva I.N., Berdnik O.B., Fel Y.A., Krivina L.A.

(Rus)

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)

Modelling of an ejector for turbine aeroengines for application in performance synthesis tools

Georgi J., Staudacher S., Falaleev S.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 8, No 3-3 (2009): Special Issue

Theoretical calculation approach of gas turbine engines compressor characteristic line

1 1.

(Rus)

The optimization of the turbine blade-disk interlock of the type “fir tree”

1 1., 1 1.

(Rus)

Correlation and regression model for the assessment of circular non-uniformity of the gas temperature field at the outlet of small gas turbine engine combustion chambers

Lukachev S.V., Abrashkin V.Y., Lansky A.M., Matveev S.G.

(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 2 (2020)

Gas turbine engine dynamic model based on variable-memory LSTM architecture

Kuznetsov A.V., Makaryants G.M.

(Rus)

Vol 10, No 6 (2011)

Choise of the range and levels of varying the factors of the experiment plan for testing single-stage ultralow power turbine

Grigoryev V.A., Radko V.M., Kalabukhov D.S.

(Rus)

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 2 (2019)

Theory of gas turbine engine optimal gas generator

Grigoriev A.V., Kosmatov A.A., Rudakov О.A., Solovieva A.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 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 15, No 4 (2016)

Application of structure-energy failure theory for determining the probability of failure and durability of turbine and compressor blades of aircraft engines

Chernyaev A.I., Trefilov V.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

Experimental determination of thermal-fatigue life of turbine blades with various coatings made of an advanced heat resistant nickel alloy

Bychkov N.G., Nozhnitsky Y.A., Khamidullin A.S., Pershin A.V., Avrutsky V.V.

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

Causes of failures of rolling bearings

Zvonarev S.L., Zubko A.I.

(Rus)

Gas turbine engine simulation strategy in CAE systems

Krivcov A.V.

(Rus)

Approaches to modeling work of gas turbine engine`s core as a connected task

Krivcov A.V., Shabliy L.S., Baturin O.V.

(Rus)

Increase durability of gas turbine disks

Nikishov O.V., Krutsilo V.G.

(Rus)

Methodology complex of hardware-in-the-loop functional modelling of gas turbines and its systems

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

(Rus)

Electronic model of turbine drive flow for its direct optimization

1 1.

(Rus)

Pressure-gain combustion and its potential for gas turbine engine enhancement

Lutoschkin E.V., Rose M.G., Staudacher S.

(Rus)

Evaluating the possibility of using low-temperature thermal energy in liquefied natural gas complexes

Dovgjallo A.I., Sarmin D.V., Uglanov D.A., Shimanov A.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 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)

Method for optimizing mass and size characteristics of a high-pressure turbine disk

Siluyanova M.V., Grunin A.N., Alendar A.D., Kandaurov S.K.

(Rus)

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

Automated system for measuring geometric parameters of turbine blades in production conditions

Aleksentsev E.I., Shavrin P.A., Fedoseev O.B.

(Rus)

On the issue of research of the properties of the heat-resistant nickel single-crystal superalloys

Tikhomirova E.A., Zhivushkin A.A., Getsov L.B., Rybnikov A.I.

(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 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 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)

Method of vibration diagnostics of aerodynamic and aeroelastic oscillations in gas turbine engine compressor

Posadov V.V., Remizov A.E.

(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 14, No 1 (2015)

Possibility of using a bi-directional impulse turbine in a thermo-acoustic engine

Dovgjallo A.I., Shimanov A.A.

(Rus)

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

Problems of ultralow power turbine design in a turbine drive system

Kalabuhov D.S., Grigoryev V.A., Rad’ko V.M.

(Rus)

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

Thermoplastic strengsening of blades aircraft gas turbine engines

Krotinov N.B.

(Rus)

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)

Problem of multistage compressor optimization while designing perspective gas turbine engines

Shabliy L.S.

(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)

Simulation of aircraft multistage axial turbine working processes taking into account over-shroud leakage flows and blading inflows

Baturin O.V., Popov G.M., Kolmakova D.A.

(Rus)

Estimate of key parameters of a gas turbine engines with application of the modelling procedure of the equilibrium state of homogeneous mixture of hydrocarbon fuel combustion products

Boldyrev O.I., Gorynov I.M.

(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)

The calculated study of fluid structure in a hub an axial aviation turbine

1 1., 1 1.

(Rus)

About the thermal protection of the oil cavities for designing gas turbine engines

Tryanov A.Y., Grishanov O.A., Vinogradov A.S.

(Rus)

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)

Conditions of compatibility of compressor and turbine used as part of a gas generator required to ensure turbine operability

Grigoriev A.V., Ilyushin M.Y., Mitrofanov V.A., Rassokhin V.A., Rudakov O.A., Solovieva A.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 19, No 1 (2020)

Algorithm for predicting the vibrational state of a turbine rotor using machine learning

Bolotov M.A., Pechenin V.A., Pechenina E.J., Ruzanov N.V.

(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)

Development of elements and parameters of LNG fuel system with cryogenic piston pump and gas receiver for road gas turbine locomotive

Bukin V.A., Rudenko V.F.

(Rus)

Vol 18, No 1 (2019)

Application of additive technology of selective laser melting (SLM) in designing a low emission combustion chamber of a gas turbine plant

Yeliseev Y.S., Fedorchenko D.G., Golanov S.P., Tsibisov Y.I., Tyulkin D.D., Vorotyntsev I.E., Ivchenko A.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 2 (2017)

Assessment of gas turbine engine airfoil surface microstructure

Nosov N.V., Abramov A.D., Kosulin S.I.

(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 10, No 5 (2011)

Research of toxic substances emission during water injection into a combustion chamber

Mingazov B.G., Mukhametgaliev T.H.

(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 5-2 (2014): Special Issue

Experimental research of heat exchange in a plane channel using the regular thermal regime mrthod with different Biot numbers

Kolesova E.G., Veretennikov S.V., Zhornik M.N.

(Rus)

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

Installation for strengthening local thermoplastic turbulent disc

Krutsilo V.G., Nikishov O.V.

(Rus)

Working conditions analysis of rotor supports bearings in aviation gas turbine engines and energetic units structure

Zrelov V.A., Makarchuk V.V., Prodanov M.E., Sudarev A.A.

(Rus)

MR vibration dampers development to reduce vibration and noise in gas turbine locomotive and their equivalent vibration tests

Ermakov A.I., Lazutkin G.V., Parovay F.V., Troynikov A.A.

(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)

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

Aerodynamic improvement of GTE compressors by space profiling of blade vanes

Gerasimenko V.P., Shelkovsky M.Y.

(Rus)

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)

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)

Optimization characteristics of rotor-support system from NK-14ST free power turbine with consider statics and dynamics propertys

1 1., 1 1.

(Rus)

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)

Criteria of discrete phase control of blade working condition and their feasibility in systems of turbine driven set automatic control

Danilin A.I., Tchernyavsky A.Z.

(Rus)

Thermal state of a groind-use gas turbine engine stator

Grechishnikov O.V., Balakin A.Y., Roslyakov A.D.

(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)

Formation of film cooling on the turbine blade back and pressure side in the case of using V-shaped dimples

Lebedev V.V., Lebedev O.V., Remizov A.E.

(Rus)

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

Determination of a rational combination of the radial turbine basic parameters with an allowance for strength, technological and other constraints

Baturin O.V., Shabliy L.S.

(Rus)

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 16, No 2 (2017)

Micro gas turbine engine imitation model

Kuznetsov A.V., Makaryants G.M.

(Rus)

Vol 15, No 4 (2016)

Development of an exhaust air turbine engine

Yeliseev Y.S., Fedorchenco D.G., Tsibizov Y.I., Tyulkin D.D., Tkachenko A.Y.

(Rus)

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

Conversion of gas turbine engine oil system

Boev A.A., Grishanov O.A.

(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 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

Research of gas turbine engine operation in dust-filled atmosphere

Abdullin B.R., Akmaletdinov R.G., Goumerov K.S., Nigmatullin R.R.

(Rus)

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

Combined calculation of gas generators of small GTE in package ANSYS CFX

Matveev S.G., Orlov M.Y., Matveev S.S., Zinkovskii V.S., Krivtsov A.V.

(Rus)

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)

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

Defects of shrouded blade platforms of high-temperature gas turbines

Belousov A.I., Nazdrachyov S.V.

(Rus)

Vortex effect and intensification of heat and mass transfer in cell energy technology

Piralishvily S.A., Veretennikov S.V.

(Rus)

Vol 9, No 1 (2010)

Compulsory ignition of fuel-air mixture in small-sized gas turbine engine combustion chambers

1 1., 1 1., 1 1.

(Rus)

Features of designing gas turbine of complex cycle GT24

1 1.

(Rus)

Estimation the factors, make the greatest influence on reliability parametres of a GTD disk with a glance sudden failures

Belousov A.I., Gritsin A.V.

(Rus)

Vol 8, No 1 (2009)

Problems of making auxiliary gas turbine engines with gas bearing rotors

Ponomaryov B.A., Gavrilov V.V.

(Rus)