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Use of the dynamic programming method for solving tasks of GTE management optimization using the aircraft efficiency criteria
Tkachenko A.Y., Kuzmichev V.S.
Modelling of an ejector for turbine aeroengines for application in performance synthesis tools
Georgi J., Staudacher S., Falaleev S.V.
Compulsory ignition of fuel-air mixture in small-sized gas turbine engine combustion chambers
1 1., 1 1., 1 1.
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.
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.
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.
Theory of gas turbine engine optimal gas generator
Grigoriev A.V., Kosmatov A.A., Rudakov О.A., Solovieva A.V.
Оptimization of gas turbine aircraft engine control throughout the engine service life
Gurevich O.S., Golberg F.D., Smetanin S.A., Trifonov M.E.
Assessment of gas turbine engine airfoil surface microstructure
Nosov N.V., Abramov A.D., Kosulin S.I.
Method of vibration diagnostics of aerodynamic and aeroelastic oscillations in gas turbine engine compressor
Posadov V.V., Remizov A.E.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
Development of blend composition of aviation kerosene surrogate for the simulation of workflow of gas turbine engine combustion chamber
Matveev S.G.
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.
Improvement of friction units of power plants by aplying ceramic composite spray coatings
Siluyanova M.V., Fertikov A.O.
Micro gas turbine engine imitation model
Kuznetsov A.V., Makaryants G.M.
Investigation of the causes of crack origination in the inner casing of NK-86 gas turbine engine combustion chamber
Kocherova Е.Е.
Selection of optimal configuration and workflow parameters of autonomous micro gas turbine plant
Baturin O.V., Smirnova Y.D.
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.
Construction of a blade beam finite element as a component of the blade disk rotary-symmetrical system
Davydov D.P.
The calculated study of fluid structure in a hub an axial aviation turbine
1 1., 1 1.
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.
Problems of making auxiliary gas turbine engines with gas bearing rotors
Ponomaryov B.A., Gavrilov V.V.
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.
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.
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.
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.
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.
Using the «virtual engine» software in automatic control system of gas turbine engine
Golberg F.D., Gurevich O.S., Petukhov A.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.
Modification of the starter turbine disk for blade containment certification tests
Karimbaev K.D., Sapronov D.V.
Experience of operational development of starting characteristics of the APU combustion chamber
Chechulin A.Y.
Computer-aided system of virtual gas turbine engine testing
Tkachenko A.Y., Rybakov V.N., Krupenich I.N., Ostapuk Y.A., Filinov E.P.
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.
A technique to estimate efficiency of turbine underplatform friction dampers
Nikhamkin M.S., Sazhenkov N.A.
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.
Rotor in gas bearings dynamics experiment-calculated investigation
Temis Y.M., Temis M.Y., Egorov A.M., Gavrilov V.V., Ogorodov V.N.
Seal designing in a structure of the cooling system in gas turbine engine
Vinogradov A.S., Myatlev A.S.
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