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Study of the efficiency of the application of gas dynamic stabilization of the flame in a current engine
Belonozhkin V.V., Teslya D.N.
JSC “ODK” experience in implementing digital twin technologies in the design of gas turbine engines
Vinogradov K.A., Nikulin A.S., Shmotin Y.N.
Series of diagnostic indicators of gearbox teeth wear in aircraft gas turbine engines
Sundukov A.Y., Shakhmatov Y.V.
Influence of pad geometry and method of oil supply on the thermal state of GTE rotor tilting-pad journal bearing
Parovay E.F.
Standardization of diagnostic indicators of gearbox teeth wear in aircraft gas-turbine engines
Sunduckov A.Y., Shakhmatov Y.V.
Analysis of low-thrust liquid rocket engines with a methane air pump unit
Ivanov A.I., Kositsin I.P., Borisov V.A.
Introduction to the problem of calculating the parameters of the mixing chamber of an afterburning bypass engine
Karev O.D.
Life of gas turbine engine components under corrosive exposure
Pivovarova M.V., Gladkiy I.L.
Calculation of lubricant flow in the slide bearing of the aviation engine reducer
Siluyanova M.V., Fertikov A.О.
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.
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.
Peculiarities of computer modeling of the working process in small gas turbine engines
Kuz'michev V.S., Tkachenko A.Y., Ostapyuk Y.A.
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.
Computer-aided system of virtual gas turbine engine testing
Tkachenko A.Y., Rybakov V.N., Krupenich I.N., Ostapuk Y.A., Filinov E.P.
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.
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.
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.
Seal designing in a structure of the cooling system in gas turbine engine
Vinogradov A.S., Myatlev A.S.
Mathematical model of turbofan engine weight estimation taking into account the engine configuration and size
Avdeev S.V.
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.
Development of blend composition of aviation kerosene surrogate for the simulation of workflow of gas turbine engine combustion chamber
Matveev S.G.
Evaluation of turbine rotor blade life taking into account static and thermal cyclic loading
Badamshin I.K.
Assessment of gas turbine engine airfoil surface microstructure
Nosov N.V., Abramov A.D., Kosulin S.I.
Research of hydrodynamic processes in the lubrication system of gas turbine engines
Gulienko A.I., Shchurovskiy Y.M.
Rotary isochoric combustion chamber of a gas turbine engine
Porshnev V.A.
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.
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.
Construction of a blade beam finite element as a component of the blade disk rotary-symmetrical system
Davydov D.P.
Project of 30 000 h.p. power gas turbine
Zrelov V.A.
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.
Efficiency of technical workings out in batch production GTE
Aleksentsev E.I., Shitarev I.L., Kurbatov V.P., Gritsenko E.A.
Influence of the stressed state of the surface layer on the endurance of gas turbine engine compressor blades
Sazonov M.B., Solovatskaya L.V.
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.
Micro gas turbine engine imitation model
Kuznetsov A.V., Makaryants G.M.
Using the «virtual engine» software in automatic control system of gas turbine engine
Golberg F.D., Gurevich O.S., Petukhov A.A.
Modification of the starter turbine disk for blade containment certification tests
Karimbaev K.D., Sapronov D.V.
Design of the gas turbine engine rotor wheel with ceramic blades
Sapronov D.V., Reznik S.V.
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.
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.
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.
Pressure-gain combustion and its potential for gas turbine engine enhancement
Lutoschkin E.V., Rose M.G., Staudacher S.
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.
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.
Gas turbine engine rotor bearings electrical current damage on the base of NK-family engines for electrical generator drive
Nazdrachev S.V.
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.
Improvement of friction units of power plants by aplying ceramic composite spray coatings
Siluyanova M.V., Fertikov A.O.
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.
The influence of booster design features on aicraft engine fan tonal noise
Khaletskiy Y.D., Korzhnev V.N., Pochkin Y.S.
Vortex gas wind-driven power plant for supplying compressor stations with electrical energy
Biryuk V.V., Zubrilin I.A., Krasnorutskiy A.S.
Check and prediction of gas-turbine engine’s technical state
Zotin N.A.
Robust research of the fuzzy logic controllers using a fuel flow control loop of the gas-turbine engine as an example
Chicherova E.V.
Aerodynamic improvement of GTE compressors by space profiling of blade vanes
Gerasimenko V.P., Shelkovsky M.Y.
1
1 1., 1 1.
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.
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.
Optimization of fuel distribution in the afterburner of a gas turbine engine
Nelyubin V.R.
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.
Improvement of gas turbine engines due to isothermal expansion in the turbine
Muraeva M.A., Gorjunov I.M.
Investigation of the causes of crack origination in the inner casing of NK-86 gas turbine engine combustion chamber
Kocherova Е.Е.
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.
Thermoplastic strengsening of blades aircraft gas turbine engines
Krotinov N.B.
Application of thermoplastic hardening for restoration of fatigue durability of gas turbine disks
Vishnyakov M.A.
Method of calculating GTE gas-thermodynamic parameters with blade row description of an axial multistage compressor
Boyko L.G., Karpenko E.L., Akhtemenko U.F.
A separator skidding in the cylindrical roller bearing between shafts of the gas turbine engine
1 1., 1 1., 1 1.
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.
Gas turbine engine dynamic model based on variable-memory LSTM architecture
Kuznetsov A.V., Makaryants G.M.
On selection of automatic control system for crvogenic fuel gas turbine engine
Bukin V.A.
Оptimization of gas turbine aircraft engine control throughout the engine service life
Gurevich O.S., Golberg F.D., Smetanin S.A., Trifonov M.E.
Methods of evaluating low-cycle fatigue of gas turbine engine parts exemplified by a high-pressure turbine cover plate
Kocherova E.E.
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.
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.
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.
Gas turbine engine designing on the basis of a unified gas generator
Rybakov V.N.
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.
Operational testing of thermoplastic reinforced blades
Krutsilo V.G., Krotinov N.B.
Theoretical calculation approach of gas turbine engines compressor characteristic line
1 1.
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.
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.
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.
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.
Development of a new collector device for gas turbine engine afterburner
Teslya D.N., Mayatsky S.A., Grasko T.V.
Unstady heat-mass-transfer and fuel distributions in flows downstream the gas-dynamic flame holder
Tretyakov V.V., Sviridenkov A.A.
Testing of gas turbine engine bearing oil supply through an oil-catch ring
Boev A.A., Petrukhin A.G., Mikhailov A.A.
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.
Optimization features of the working process parameters of bypass engine on the basis of given gas generator
Rybakov V.N.
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.
Modelling of an ejector for turbine aeroengines for application in performance synthesis tools
Georgi J., Staudacher S., Falaleev S.V.
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.
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.
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.
Ensuring permissible level of gas turbine dynamic loading in operation by means of standard engine control devices
Chervonyuk V.V., Korovin B.B.
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.
Selecting a squeeze film damper model for solving problems of gas turbine engine rotor dynamics
Leontiev M.K., Kutakov M.N.
Method of vibration diagnostics of aerodynamic and aeroelastic oscillations in gas turbine engine compressor
Posadov V.V., Remizov A.E.
Conversion of gas turbine engine oil system
Boev A.A., Grishanov O.A.
Development of the technology of diagnostics of turbo-jet aviation engines by a filtering element with a diagnostic layer
Drokov V.V., Drokov V.G., Muryshenko V.V., Mukhutdinov F.I., Khaliullin V.F.
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.
Use of the dynamic programming method for solving tasks of GTE management optimization using the aircraft efficiency criteria
Tkachenko A.Y., Kuzmichev V.S.
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.
Features of the new gas turbine aviation engines theory course
Mingazov B.G., Kosterin V.A., Varsegov V.L.
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