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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)

Estimation of parameters of a pulse detonation engine (РDЕ)

Anakin A.T., Tsybizov Y.I.

(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)

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 3-3 (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)

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 2 (2018)

Development of a multiuser system web-interface as a tool of using mathematical packages for solving engineering tasks

Danilenko A.N., Zhdanov I.A.

(Rus)

Vol 16, No 1 (2017)

Evaluation of low cycle fatigue based on the use of Coffin-Manson dependence under zero-to-“soft” loading cycle

Pavlov V.F., Kirpichyov V.A., Kocherova E.E., Zlobin A.S.

(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 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)

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 13, No 5-4 (2014): Special Issue

Research of the validity of forecasting low cycle durability of gas turbine engine parts based on Manson’s equation

Porter А.M., Bukatyi S.A., Leshin D.P.

(Rus)

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

Experimental investigation of a small-sized centrifugal compressor for a closed-brayton cycle gas turbine power system

Arbekov A.N., Novitskiy B.B.

(Rus)

Approaches to parametric models of blade machines formation

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

(Rus)

A technique to estimate efficiency of turbine underplatform friction dampers

Nikhamkin M.S., Sazhenkov N.A.

(Rus)

Dependence of required turbine inlet temperature at cruise mode of long-term flight on bypass ratio

Rybakov V.N.

(Rus)

Vol 13, No 2 (2014)

Discrete phase converters moving elements rotating units power units

Danilin A.I., Grechishnikov V.M.

(Rus)

Effect of cavity width on performance of pre-swirl systems

Didenko R.A., Karelin D.V., Ievlev D.G., Lebedev V.V., Belousova E.V.

(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)

Way of increase in efficiency of cycle gas turbine units

1 1.

(Rus)

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

Goryunov A.I., Goryunov I.M.

(Rus)

Vol 7, No 3 (2008): Special Issue

Calculated study of tangential inclination of nozzle vanes influence on gas-dynamic efficiency of axial turbine stage

Baturin O.V., Matveev V.N.

(Rus)

Vol 12, No 4 (2013)

Improvement of the quality of the surfaces of monowheel blades of liquid rocket engine turbopump assemblies

Mozgov S.A., Panov D.V., Saushkin B.P.

(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)

Comparative analysis of facilities for the implementation of thermoplastic hardening blades of gas turbine engines and pumping units

Karpov A.V.

(Rus)

Experiment-calculated research of the influence of the shot-peening strengthening upon the low-cycle fatigue of the gas turbine parts with the stress concentrator

Porter A.M., Bukaty S.A., Leshin D.P., Bukaty A.S.

(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 2 (2018)

Improvement of friction units of power plants by aplying ceramic composite spray coatings

Siluyanova M.V., Fertikov A.O.

(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

Optimization of the workflow of multistage axial turbines with platforms

Matveev V.N., Baturin O.V., Popov G.M., Goryachkin E.S.

(Rus)

Vol 10, No 5 (2011)

The concept of matching the joint operation of the combustion chamber, the compressor and the turbine

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

(Rus)

Vol 13, No 5-4 (2014): Special Issue

Development of the construction of a gas turbine engine vane with built-in vortex tubes

Veretennikov S.V., Barinov S.N.

(Rus)

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

Development of a prototype of a multi-loop closedbrayton cycle gas turbine power system

Arbekov A.N., Novitskiy B.B.

(Rus)

Gas turbine engine designing on the basis of a unified gas generator

Rybakov V.N.

(Rus)

Selection of optimal configuration and workflow parameters of autonomous micro gas turbine plant

Baturin O.V., Smirnova Y.D.

(Rus)

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

The defectoscopy of the fatigue cracks in the gas turbine parts by means of eddy-current method

Porter A.M., Bukatyi S.A., Leshin D.P., Vasilchuk M.V., Galickyi A.A.

(Rus)

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 13, No 2 (2014)

Circuit design receipt autodynes signal to converter displacement parameters elements rotating parts of turbune unit

Danilin A.I., Gretskov A.A.

(Rus)

Effect of radial location of nozzles on width on performance of pre-swirl systems

Didenko R.A., Karelin D.V., Ievlev D.G., Lebedev V.V.

(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)

Probabilistic estimate of compressor blades durability to foreign object damage

1 1., 1 1.

(Rus)

Seal designing in a structure of the cooling system in gas turbine engine

Vinogradov A.S., Myatlev A.S.

(Rus)

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 20, No 4 (2021)

Choice of gas temperature at the turbopump turbine inlet

Ivanov A.V.

(Rus)

Vol 19, No 3 (2020)

Method of coordinating joint operation of air starter and auxiliary power unit and determining the gas turbine engine starting time

Popov G.M., Baturin O.V., Novikova Y.D., Zubanov V.M., Volkov A.A., Korneeva A.I.

(Rus)

Vol 18, No 3 (2019)

Life of gas turbine engine components under corrosive exposure

Pivovarova M.V., Gladkiy I.L.

(Rus)

Bases of methodology of maintenance of system safe operation of engines at all stages of life cycle

Grigoriev V.A., Kuznetsov S.P.

(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)

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 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 15, No 4 (2016)

Morphological characteristics of the intermetallic phase of heat resisting nickel alloys

Kirikov S.V., Perevezentsev V.N., Tarasenko Y.P.

(Rus)

Vol 15, No 3 (2016)

Laser powder weld reconditioning of gas turbine engine blades

Korsmik R.S., Turichin G.A., Klimova-Korsmik O.G., Zemlyakov E.V., Babkin K.D.

(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)

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 5-3 (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)

Optimization features of the working process parameters of bypass engine on the basis of given gas generator

Rybakov V.N.

(Rus)

Computational research of multistage turbine flow taking into account flow spatial structure and associated volumes

Baturin O.V., Senchev M.N., Dzhibilov P.T.

(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)

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)

Operational testing of thermoplastic reinforced blades

Krutsilo V.G., Krotinov N.B.

(Rus)

Rotor in gas bearings dynamics experiment-calculated investigation

Temis Y.M., Temis M.Y., Egorov A.M., Gavrilov V.V., Ogorodov V.N.

(Rus)

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

A separator skidding in the cylindrical roller bearing between shafts of the gas turbine engine

1 1., 1 1., 1 1.

(Rus)

the research of the influence of the maximal stress duration in the cycle of loading upon the low-cycle fatigue and the long-term strength of the turbine shaft made of the material ЭИ 961-Ш

1 1., 1 1., 1 1.

(Rus)

The oretical substantiation of the constructive scheme of the air-gas tract rinsing device for GTE

Silaev B.M., Mal’tsev E.N.

(Rus)

Development of an algorithm of design calculation of a combustion chamber for microturbine electric power plants

Matveev S.G., Abrashkin V.Y., Orlov M.Y., Lansky A.M., Makarov N.S., Matveev S.S., Anisimov M.Y.

(Rus)

Vol 19, No 2 (2020)

Technology of low-emission fuel combustion and conceptual structure of the combustion chamber of a gas-turbine power plant

Tsybizov Y.I., Tyulkin D.D., Vorotyntsev I.E.

(Rus)

Vol 18, No 3 (2019)

Mathematical model for calculating the mass of a heat exchanger in problems of optimizing the parameters of the working process of aircraft gas turbine engines

Kuz'michev V.S., Omar H., Tkachenko A.Y., Bobrik A.A.

(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)

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)

Vol 10, No 6 (2011)

Planning a factorial experiment for testing a single-stage ultralow power turbine

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

(Rus)

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

Analysis of the possibility of using topology optimization in the design of uncooled turbine rotor blades

Vasilyev B.E., Magerramova L.A.

(Rus)

Vol 14, No 2 (2015)

Experience of operational development of starting characteristics of the APU combustion chamber

Chechulin A.Y.

(Rus)

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

Development of methods of carrying out experimental research of measurement errors for sets of geometrical parameters on NC equipment as in the case of a turbine disk

Bolotov M.A., Alexeev V.P., Pronichev N.D.

(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)

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)