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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.
Using the energy of gas differential pressure in electromagnetic injectors for improved breathing of spark-ignition internal combustion engine cylinders
Shishkov V.A.
Vortex cleaning of fuel tank pressurant gas
Biryuk V.V., Shimanov A.A., Onoprienko D.A., Smorodin A.V., Shepelev A.I.
Features of design calculation of compressor spool flow path of a twin-shaft gas turbine engine core on the basis of 1D and 2D models of their working process
Matveev V.N., Goriachkin E.S., Popov G.M., Baturin O.V., Kudryashov I.A.
Study of the efficiency of the application of gas dynamic stabilization of the flame in a current engine
Belonozhkin V.V., Teslya D.N.
Verification of a transonic stage CFD model for assessing the erosion wear influence on the operation of the axial compressor
Blinov V.L., Zubkov I.S.
Investigation of the influence of broadband mechanical disturbances on the quality of recording interference patterns of GTE-wheel oscillations using a digital speckle pattern interferometer
Ivchenko A.V., Safin A.I.
Resistance of products made of steel 20GL to sulfide stress corrosion cracking
Blazhnov N.M., Borisenkova E.A., Khardin M.V.
Development and research of a gas stamping device for making hollow products from a pipe billet
Botashev A.Y., Bayramukov R.A., Bisilov N.U., Dzhumanazarov E.K., Malsugenov R.S.
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.
Neural network controller of a gas turbine plant low emission combustor
Avgustinovich V.G., Kuznetsova T.A., Sukharev A.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.
Method of scanning thin surfaces in repairing gas turbine blades
Kotlyar D.I., Lomanov A.N.
On selection of automatic control system for crvogenic fuel gas turbine engine
Bukin V.A.
Project of 30 000 h.p. power gas turbine
Zrelov V.A.
JSC “ODK” experience in implementing digital twin technologies in the design of gas turbine engines
Vinogradov K.A., Nikulin A.S., Shmotin Y.N.
Validation of the “stage – diffuser” system numerical study and its use for design modernization
Cherkasova M.G., Semakina E.Y., Chernikov V.A.
Comparative analysis of facilities for the implementation of thermoplastic hardening blades of gas turbine engines and pumping units
Karpov A.V.
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.
Influence of pad geometry and method of oil supply on the thermal state of GTE rotor tilting-pad journal bearing
Parovay E.F.
Joint work of units and characteristics of elements gas the equipment for the engine of internal combustion with spark ignition
Shishkov V.A., Lesnih U.I.
Application of open-source software for industrial problems of vehicle lift-off gas dynamics
Abdurashidov T.O., Osipov A.V., Korchagova V.N., Kraposhin M.V., Smirnova Y.V., Strizhak S.V.
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.
Gasdynamic and strength improvement of the axial flow turbine of a helicopter gas turbine engine
Goriachkin E.S., Popov G.M., Matveev V.N., Shcherban A.I., Kudryashov I.A., Melnikov S.A.
Bases of methodology of maintenance of system safe operation of engines at all stages of life cycle
Grigoriev V.A., Kuznetsov S.P.
Shock wave profiles in relaxing gas with external energy source
Anchikov D.A., Galimov R.N., Zavershinskii D.I., Makaryan V.G., Molevich N.E.
Research of the mechanism of shock-inertial deposition of dispersed particles from a gas flow
Usmanova R.R., Zhernakov V.S.
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.
Structure and physico-mechanical properties of heat resistant gazoplazmennyh coating NiCrCoAlY/ZrO2 for turbine blades of gas turbine engines
Tarasenko Y.P., Tsareva I.N., Berdnik O.B., Fehl Y.A.
Gas turbine engine designing on the basis of a unified gas generator
Rybakov V.N.
Development of a mathematical model of the internal structure of a granular heat accumulator for launching a mono-fuel gas generator
Zrelov V.A., Lykin A.Y.
Series of diagnostic indicators of gearbox teeth wear in aircraft gas turbine engines
Sundukov A.Y., Shakhmatov Y.V.
Vortex gas wind-driven power plant for supplying compressor stations with electrical energy
Biryuk V.V., Zubrilin I.A., Krasnorutskiy A.S.
Optimization features of the working process parameters of bypass engine on the basis of given gas generator
Rybakov V.N.
Fluctuations of pressure in rail gas injection of engines with spark ignition
Shishkov V.A.
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.
Influence of the loading parameter on the efficiency ofa three-stage turbine of turbojet bypass engine
1 1., 1 1.
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.
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.
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