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Authors
Research of the dynamics of condensed product deposition
Tsaplin S.V., Bolychev S.A.
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.
Application of gas analyzers for the control of fuel in the air environment of rocket and space industry enterprises
Bulgakov A.B., Vashchuk S.P., Panshin R.A.
Operation of an electronic system of control for spark-ignition gas fuel internal combustion engines in ignition misses
Shishkov V.A.
Dynamik experimental researches of the face gas dynamic seal
Novikov D.K., Balyakin V.B., Sedov 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.
Elimination of gas dynamic resonance modes of vibration loads of gas distribution station pipeline fitting
Shabanov K.U., Kryuchkov A.N., Ermilov M.A., Balyaba M.V.
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.
Key focus areas of samara state aerospace university research and education center of gasdynamic research
Matveev V.N., Anisimov M.Y.
A technique to estimate efficiency of turbine underplatform friction dampers
Nikhamkin M.S., Sazhenkov N.A.
Application of thermoplastic hardening for restoration of fatigue durability of gas turbine disks
Vishnyakov M.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.
Algorithm of adaptation of an electronic control system of internal combustion engines to various chemical compositions of gas fuel
Shishkov V.A.
Applying Lagrange’s approach to solving a one-dimensional problem of wave propagation in gas in linear formulation
Nikonov V.V., Shakhov V.G.
Research of laws of interaction of components in a liquid phase self-igniting liquid rocket fuel
1 1., 1 1.
Seal designing in a structure of the cooling system in gas turbine engine
Vinogradov A.S., Myatlev A.S.
Uniform and equidistant ways of structured computation grigd creation for CFD problems
Yefimow A.N., Matveev V.N.
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.
Professor A.P. Merkulov’ role in the process of research and development of the vortex effect
Biryuk V.V., Lukachev S.V., Volov V.T., Pirallishvili S.A.
Gas turbine engine dynamic model based on variable-memory LSTM architecture
Kuznetsov A.V., Makaryants G.M.
Experimental research of thermal yet influence of staff LTRE upon the construction models of airspace devices
Shustov S.A.
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.
Theoretical and experimental studies of a gas stamping device with a piston pressure multiplier
Botashev A.Y., Bayramukov R.A.
Schemes, parameters, work process, characteristics and structure of long-range interception aircraft engines
Kovalev A.V., Sanin V.N., Krivenok A.G., Korolenko V.V.
Methods of evaluating low-cycle fatigue of gas turbine engine parts exemplified by a high-pressure turbine cover plate
Kocherova E.E.
Frequency characteristics of a coaxial gas damper for booster feed line
Odinokov D.A., Gimadiyev A.G.
Procedure of designing a pilot operated gas pressure regulator for launch vehicle fuel tanks
Gimadiev A.G., Sverbilov V.Y., Stadnik D.M.
Testing of gas turbine engine bearing oil supply through an oil-catch ring
Boev A.A., Petrukhin A.G., Mikhailov A.A.
Research of toxic substances emission during water injection into a combustion chamber
Mingazov B.G., Mukhametgaliev T.H.
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.
Research of gas turbine engine operation in dust-filled atmosphere
Abdullin B.R., Akmaletdinov R.G., Goumerov K.S., Nigmatullin R.R.
Heat-shielding zirconium dioxide coating on an intermetallic substrate obtained by the method of high-energy plasma spraying for gas-turbine engine turbine blades
Tarasenko Y.P., Tsareva I.N., Berdnik O.B., Fel Y.A., Fedorchenko D.G.
Causes of failures of rolling bearings
Zvonarev S.L., Zubko A.I.
An experimental technique for efficiency assessment of ring dampers for gas turbine engine blisk
Nikhamkin M.S., Balakirev A.A., Voronov L.V.
Determining the angle of advance of ignition when switching from petrol to gas depending on fuel mixture burning rate
Shishkov V.A.
Approaches to modeling work of gas turbine engine`s core as a connected task
Krivcov A.V., Shabliy L.S., Baturin O.V.
Experimental investigation of turbulence of influence of the compressor’s out flow parameters on the hydraulics parameters resistance of separation diffuser of combustion chamber
Guryanova M.M.
Designing GTE on the basis of versatile gas generator small dimension
1 1., 1 1.
Optimization characteristics of rotor-support system from NK-14ST free power turbine with consider statics and dynamics propertys
1 1., 1 1.
The oretical substantiation of the constructive scheme of the air-gas tract rinsing device for GTE
Silaev B.M., Mal’tsev E.N.
Increasing efficiency of pressurization of the rocket tanks in the flight
Biryuk V.V., Kapitonov V.A., Smorodin A.V.
Method of calculation and analysis of gas flow aerodynamic indices in a vortex wind power plant
Biryuk V.V., Uglanov D.A., Gorshkalev A.A., Bolshov D.V., Krasnorutskiy A.S., Lapshina V.A., Chertykovtsev P.A.
Gas-dynamic losses in the flow part of the channel charge of a solid-propellant rocket engine
A. N. Sabirzyanov A.N., Khamatnurova C.B., Kuzmin V.V.
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.
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.
Gas turbine engine rotor bearings electrical current damage on the base of NK-family engines for electrical generator drive
Nazdrachev S.V.
Diagnostics of state gas-fluid of flows in the field of cross vibration
Limanova N.I., Levkin U.S.
Development of the active gas generator for high altitude firing test benches
Salich V.L.
Estimating the efficiency of a bypass turbojet engine on the basis of a serial gas generator as a part of the power plant of a high-altitude unmanned aerial vehicle
Zinenkov Y.V., Lukovnikov A.V., Popov A.V., Nechaev V.N.
Development of a new collector device for gas turbine engine afterburner
Teslya D.N., Mayatsky S.A., Grasko T.V.
Improvement of gas turbine engines due to isothermal expansion in the turbine
Muraeva M.A., Gorjunov I.M.
The influence of booster design features on aicraft engine fan tonal noise
Khaletskiy Y.D., Korzhnev V.N., Pochkin Y.S.
Conversion of gas turbine engine oil system
Boev A.A., Grishanov O.A.
Construction of detailed kinetic mechanisms of forming for five ring PAH and their reduction for use in modern CAE systems
Matveev S.G., Chechet I.V.
Study of characteristics of the launch vehicle fuel line gas damper
Gimadiev A.G., Odinokov D.A., Stadnik D.M., Greshnyakov P.I.
Experimental investigation of a small-sized centrifugal compressor for a closed-brayton cycle gas turbine power system
Arbekov A.N., Novitskiy B.B.
Thermoplastic strengsening of blades aircraft gas turbine engines
Krotinov N.B.
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.
Gas turbine engine simulation strategy in CAE systems
Krivcov A.V.
Numerical modeling on dynamic process of injection in supersonic part of the nozzle
Yakovchuk M.S.
Simulator, algorithm and software for the computation of differential gas circuits frequency response
Igonin A.A., Gimadiev A.G.
Quasi one-dimensional model and calculation of processes in gas turbineengine combustion chambers given the heterogeneity of the combustible mixture, changes in mass, composition, temperature and stirring efficiency of the working body
Didenko A.A., Sokolov A.B.
Prospects for the forcing of gas turbine and steam power plants
Pavlova A.A.
Definition of directions of developing methods, technical decisions and means of decreasing the technogenic influence on the environment for the omplementation on board of space launch vehicles
Shatrov Y.T., Baranov D.A., Trushlyakov V.I., Kudentsov V.Y.
A separator skidding in the cylindrical roller bearing between shafts of the gas turbine engine
1 1., 1 1., 1 1.
Features of designing gas turbine of complex cycle GT24
1 1.
CFD-based modeling of oil ang gas journal bearings using commercial software packages
Pugachev A.O., Ravikovich Y.A., Ermilov Y.I., Kholobtsev D.P., Matushkin A.A.
System of pressurization of the fuel tank of a launch vehicle using the heat of generator gas
Biryuk V.V., Smorodin A.V., Shepelev A.I., Onoprienko D.A.
Mathematical model of turbofan engine weight estimation taking into account the engine configuration and size
Avdeev S.V.
Design of experiments for verification of computational life prediction methods
Samsonova O.V., Fetisov K.V., Karpman I.V., Burtseva I.V.
Features of start-up the engine of internal combustion with spark ignition on gas fuel
Shishkov V.A.
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.
Influence of the stressed state of the surface layer on the endurance of gas turbine engine compressor blades
Sazonov M.B., Solovatskaya L.V.
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.
The use of gas-dynamic flame stabilization in afterburner combustion chambers of aircraft gas turbine engines
Kolesnikov A.S., Pakhol'chenko A.A.
Morphological characteristics of the intermetallic phase of heat resisting nickel alloys
Kirikov S.V., Perevezentsev V.N., Tarasenko Y.P.
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.
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.
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.
Development of a prototype of a multi-loop closedbrayton cycle gas turbine power system
Arbekov A.N., Novitskiy B.B.
Stabilization of a pilot-operated gas pressure control valve by placing a throttle at the inlet
Stadnik D.M., Sverbilov V.Y., Makaryants G.M., Makaryants M.V.
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.
Problem of multistage compressor optimization while designing perspective gas turbine engines
Shabliy L.S.
The use of gas turbines in small-scale installations of synthetic fuels
Filipchenko S.A., Faridonov R.R., Gushchina T.V.
Aerodynamic improvement of GTE compressors by space profiling of blade vanes
Gerasimenko V.P., Shelkovsky M.Y.
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.
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