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Consideration of active forces at internal-combustion engine analysis in MSC.ADAMS environment
1 1., 1 1., 1 1.
Research of a seal work as an element of the air engine support
Vinogradov A.S., Rempel A.P.
Experimental analysis of flow separation in low thrust rocket engine nozzles with a profiled supersonic part of the nozzle
Shustov S.A.
Characteristics of the sampling instrument for measuring emissions of an aircraft gas turbine engine
Okhlobystin A.V., Lyubimov R.V., Sokolova N.N.
Introduction to the problem of calculating the parameters of the mixing chamber of an afterburning bypass engine
Karev O.D.
Development of improved performance electromagnetic valve for liquid rocket engine
Igolkin A.A., Chubenko T.A., Maksimov A.D.
Technique of conclusion the direct-flow detonation pulsing engine design to the leader position
Safronov V.V., Porshnev V.A., Zhebrakov A.S.
Research of the possibility of thermal conditions LREST using an infrared thermal imaging system
Ryzhkov V.V., Silyutin M.V.
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.
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.
Influence of the geometry fidelity of resonant sound-absorbing liner samples on their acoustic characteristics
Kustov O.Y., Khramtsov I.V., Bulbovich R.V.
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.
Methods of evaluating low-cycle fatigue of gas turbine engine parts exemplified by a high-pressure turbine cover plate
Kocherova E.E.
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.
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.
Analysis of the properties of water condensate obtained from heat engine exhaust yases
Knysh Y.A., Uglanov D.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.
Development of a single-section demonstrator rotary engine on the basis of a modern complex design procedure
Kostyuchenkov A.N., Zelentsov A.A., Semenov P.V., Minin V.P.
Research of the influence of design parameters of a 400 N-thrust low-thrust liquid rocket engine on its energy efficiency
Ageenko Y.I., Ilyin R.V., Pegin I.V.
Thermoplastic strengsening of blades aircraft gas turbine engines
Krotinov N.B.
The calculation of optimum worker frequencies of the thermoacoustic electric generator with including ready electrodynamic unit and given load
Vorotnikov G.V., Kryuchkov A.N.
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 of increase of wear resistance and vibroakusticheskikh of parameters of knots of the friction of space equipment
Gromakovsky D.G., Kovshov A.G., Kotcherov E.P., Makaryants M.V.
Optimal distribution of turboprop engine free energy between the screw and the jet with mass characteristics taken into account
Grigoriev V.A., Prokaev A.S.
Modelling of an ejector for turbine aeroengines for application in performance synthesis tools
Georgi J., Staudacher S., Falaleev S.V.
Hard & soft complex for “Angara” family launch vehicles engine system development
Partola I.S.
Some results of experimental refining of a constant volume valve combustion chamber
Bogdanov V.I., Kuznetsov S.P.
Development of turbopump unit design for hydrogen liquid-propellant rocket engines without generators developed at the design bureau of chemical automation
Dmitrenko A.I., Ivanov A.V., Rachuk V.S.
A separator skidding in the cylindrical roller bearing between shafts of the gas turbine engine
1 1., 1 1., 1 1.
Development and study of the designs of sprayers with increased speed for internal combustion engine (ice)
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Mixing parameters investigations and methods of approach to calculations and development of the thrusters with a spray-centrifugal scheme of NT and NDMH mixing on the confusion chamber wall in considered
1 1.
Problems of making auxiliary gas turbine engines with gas bearing rotors
Ponomaryov B.A., Gavrilov V.V.
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.
Increasing the sensitivity and expanding the functionality of bipolar analysis of rotary machine vibrations
Sundukov A.E., Shakhmatov Y.V.
Gas turbine engine dynamic model based on variable-memory LSTM architecture
Kuznetsov A.V., Makaryants G.M.
Life of gas turbine engine components under corrosive exposure
Pivovarova M.V., Gladkiy I.L.
Working process of gaseous fuel metallizator
Pervyshin A.N., Ryazanov A.I.
To a question of forcing up of thermal stirlings macine
Belozertcev V.N.
Method of design calculation gas-liquid jet duplex fuel nozzle with internal mixing
Egorychev V.S.
Ensuring permissible level of gas turbine dynamic loading in operation by means of standard engine control devices
Chervonyuk V.V., Korovin B.B.
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.
Engines for domestic drones: past, present and future
Cherkasov A.N., Legkonogikh D.S., Zinenkov Y.V., Panov S.Y.
Development of a new collector device for gas turbine engine afterburner
Teslya D.N., Mayatsky S.A., Grasko T.V.
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.
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.
Testing of gas turbine engine bearing oil supply through an oil-catch ring
Boev A.A., Petrukhin A.G., Mikhailov A.A.
Application of the cyclic life additivity concept for the determination of service life of aero engine disks made from powder alloys
Tumanov N.V., Lavrentyeva M.A., Vorobyeva N.A., Kalashnikova A.I.
Vortex gas wind-driven power plant for supplying compressor stations with electrical energy
Biryuk V.V., Zubrilin I.A., Krasnorutskiy A.S.
Examination of the theoretical possibility of creating a vernier electrorocket engine
Baigaliev B.E., Chernoglazova A.V., Tumakov E.A., Temnikova S.V.
50 n thrust correction engine for the "Luna-resurs" lunar module descent engine
Ageenko Y.I., Pegin I.V., Chesnokov D.V.
Simulation design, kinematic and dynamic analysis of "virtual piston engine"
Gvozdev A.S., Melentjev V.S.
Gas turbine engine designing on the basis of a unified gas generator
Rybakov V.N.
Fluctuations of pressure in rail gas injection of engines with spark ignition
Shishkov V.A.
Application of thermoplastic hardening for restoration of fatigue durability of gas turbine disks
Vishnyakov M.A.
Use of the dynamic programming method for solving tasks of GTE management optimization using the aircraft efficiency criteria
Tkachenko A.Y., Kuzmichev V.S.
Aerodynamic improvement of GTE compressors by space profiling of blade vanes
Gerasimenko V.P., Shelkovsky M.Y.
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 combined fuel draining control system for liquid oxygen and liquid hydrogen upper stage
Ivanov V.P., Partola I.S.
Analysis of economic and organizational problems in aircraft engine construction
Nikitin N.F., Cherner N.V.
Optimization methods of design-ballistic characteristics circumterraneous and interplanetary space vehicle with electrojet engines of low thrust
1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1.
Experimental determination of the side forces acting on the combustion chamber in the altitude chamber at startup
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Mathematical model of small-thrust rocket engine with gaseous oxygen and hydrogen in pulse operation
1 1.
Probabilistic estimate of compressor blades durability to foreign object damage
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.
The phase characteristic of force cutting and its role in occurrence and development of self-oscillations at sharpening not rigid details of aviation engines
Burmistrov E.V., Basyrov M.N., GiniyatuIIin R.R.
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.
Diagnostic indicators of tooth flank wear based on the analysis of tooth spectral component parameters
Sunduckov A.E.
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.
Bringing spacecraft into solar-oriented attitude by the measurements of a single-axis angular-rate sensor and an optical solar sensor
Shipov M.G., Steklova A.A., Davydov A.A.
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.
Influence in a constructive and regime parameters antechamber by operation-in the combustion chamber liquid-propellant rocket engine thrusters on hypergolic liquid propellants
Nigodjuk V.E., Sulinov A.V.
Sales training methods based on through the use of CAD / CAM / CAE systems for aero engines
Balyakin A.V., Ermakov A.I., Pronichev N.D., Chempinsky L.A.
Research of hafnium-containing defects in granular nickel EP741NP alloy using electron microscopy
Trunkin I.N., Artamonov M.A., Ovcharov A.V., Vasiliev A.L.
Numerical simulation of low liquid flow in a mixer consisting of two centrifugal swirlers
Semkin E.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.
Locally optimal control of space tug motion between the libration points of the Earth-Moon system
Starinova O.L., Fain M.K.
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.
Analysis estimation of pulse jet engine operation in detonation mode
Seyfetdinov R.B., Seyfetdinov M.B., Gafurov S.A., Shakhmatov E.V.
Vibrodiagnostics of turboprop engine gearbox wear
Sundukov A.Y., Sundukov Y.V., Plotnikov S.M.
11D58MF combined propulsion unit operating on oxygen-hydrogen fuel for an average-sized booster
Lupyak D.S., Smolentsev A.A., Sokolov B.A., Tumanin E.N., Tupitsin N.N.
Automated thermovacuum firing test facility for testing and research of workflow in low-thrust rocket engine on hypergolic propellants
Galperin R.N., Ivashin Y.S., Nigodjuk V.E., Ryzhkov V.V., Sulinov A.V.
Experimental verification of the possibility of improving the liquid propelant rocket engine performance for the “Vega” launcher upper stage
Kovalenko A.N., Pereverzev V.G., Marchan R.A., Blishun Y.V.
Modeling oil separation in the impeller of a radial-type centrifugal breather
Petrukhin A.G., Tryanov A.E.
Optimization features of the working process parameters of bypass engine on the basis of given gas generator
Rybakov V.N.
Influence of high technologies on production technological prototypes of missile engines
Kodencev S.N., Suhochev G.A.
Mathematical model and peculiarities of operating mobile robots with hybrid drives
Ilyukhin Y.V., Tatarintseva A.V.
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.
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.
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.
Methodical features of vibration tests of rotating blades using dynamic spin rigs
Nozhnitsky Y.A., Fedina Y.A., Shadrin D.V.
Quality indices of an internal combustion engine controlled by the discharge current channel
1 1., 1 1., 1 1.
Experimental development of the LRE with CCCM nozzle’s extension
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Мethod of design calculation of centrifugal emulsive duplex fuel nozzle
1 1.
Increasing efficiency of pressurization of the rocket tanks in the flight
1 1., 1 1.
Project of 30 000 h.p. power gas turbine
Zrelov V.A.
Increasing efficiency of pressurization of the rocket tanks in the flight
Biryuk V.V., Kapitonov V.A., Smorodin A.V.
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.
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