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Increasing the overall performance of a two-stroke engine with spark ignition by fuel injection
Dovgyallo A.I., Krasheninnikov S.V., Shchepetov D.A.
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.
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.
Estimation of parameters of a pulse detonation engine (РDЕ)
Anakin A.T., Tsybizov Y.I.
Algorithm of adaptation of an electronic control system of internal combustion engines to various chemical compositions of gas fuel
Shishkov V.A.
Research of influence of the thermal stream from the mid-flight liquid rocket engine on parameters of operating liquid rocket engines of small draught in the conditions of perspective razgonnogo's propulsion system of the block
Ageenko Y.I., Galperin R.N., Ivashin Y.S., Nigodjuk V.E., Ryzhkov V.V., Sulinov A.V.
Cycle parameters of an internal combustion spark-ignition gas piston engine with an electronic control system
Shishkov V.A.
Research of gas turbine engine operation in dust-filled atmosphere
Abdullin B.R., Akmaletdinov R.G., Goumerov K.S., Nigmatullin R.R.
Evaluation of the possibility of using combustion promoters in hydrocarbon fuels for perspective jet engines
Petrukhin N.V., Sergeev S.M., Prokopenko O.A., Grek M.O.
Results of experimental studies of parameters of low-thrust rocket engines operating on gaseous oxygen-hydrogen fuel
Ageenko Y.I., Lapshin E.A., Morozov I.I., Pegin I.V., Ryzhkov V.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.
Multicriterial choice of the best variant of the pulse detonation engine design for aircraft angular stabilization and orientation systems
Safronov V.V., Porshnev V.A., Zhebrakov A.S.
The influence of the shuttle effect on the intensification of heat losses in a Stirling engine
Savchenko V.A., Stolyarov S.P.
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.
Empirical metod of predicting aviation piston engine noise
Moshkov P.A.
Сalculated analysis of the influence of operation and design factors on the parameters of oxygen-hydrogen low-thrust rocket engines
Ryzhkov V.V., Morozov I.I.
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.
Optimal program of controlling continuous low thrust in the flight between noncoplanar elliptical and geostationary orbits
Fadeenkov P.V., Ishkov S.A.
Assessing the efficiency of flights to high near-earth orbits using boosters with chemical and electro-rocket engines
Ishkov S.A., Fadeenkov P.V., Balakin V.L.
Methodical features of vibration tests of rotating blades using dynamic spin rigs
Nozhnitsky Y.A., Fedina Y.A., Shadrin D.V.
50 n thrust correction engine for the "Luna-resurs" lunar module descent engine
Ageenko Y.I., Pegin I.V., Chesnokov D.V.
Using the energy of gas differential pressure in electromagnetic injectors for improved breathing of spark-ignition internal combustion engine cylinders
Shishkov V.A.
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.
Numerical simulation of tonal noise of a bypass engine fan stage
Pyatunin K.R., Arharova N.V., Remizov A.E.
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.
Evaluation of internal combustion engine cycle work using an ionic current sensor
Ivashin P.V., Ramazanov M.P., Tverdokhlebov A.Y., Shaikin A.P., Yasnikov I.S.
Aerodynamic improvement of GTE compressors by space profiling of blade vanes
Gerasimenko V.P., Shelkovsky M.Y.
Oxygen-hidrogen liquid rocket engine using turbo-pump developed for aviation hidrogen liquid two-spool turbo-jet
Ivanov A.I., Borisov V.A.
Construction of a blade beam finite element as a component of the blade disk rotary-symmetrical system
Davydov D.P.
Forecasting the individual performance capabilities of the rocket engine powerplant units at the maintanance stage
Biryuk V.V., Bronshtein V.M., Presnyakova A.S., Shatilova M.Y., Dostovalova S.S.
Analysis of economic and organizational problems in aircraft engine construction
Nikitin N.F., Cherner N.V.
Results of primary operation of NK-37 engine low emission combustion system
Bantikov D.Y., Yeliseev Y.S., Lavrov V.N., Pchelyakov A.A., Fedorchenko D.G., Tsybizov Y.I.
Flame propagation velocity and ionization in burning gasoline and methane with addition of hydrogen
Shaykin A.P., Ivashin P.V., Galiev I.R.
Determining the angle of advance of ignition when switching from petrol to gas depending on fuel mixture burning rate
Shishkov V.A.
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.
Investigation of energy parameters of small-thrust liquid rocket engines with the geometric expansion ratio of the nozzle F=200
Ageenko Y.I., Nigodyuk V.E., Ryzhkov V.V., Sulinov A.V., Shustov S.A.
Kinematic and dynamic analysis of the basic mechanism of the Wankel engine, based on its vector model
Kosenok B.B.
Check and prediction of gas-turbine engine’s technical state
Zotin N.A.
Some peculiarities of high-altitude starting of engines of the RD-33 type
Kotsyubinsky S.V., Ravikovich Y.A.
Features of start-up the engine of internal combustion with spark ignition on gas fuel
Shishkov V.A.
Peculiarities of starting a spark-ignition gas fuel internal combustion engine
Shishkov V.A.
Technology of computational analysis of the working process parameters of low-thrust rocket engines running on gaseous oxygen-hydrogen fuel with the use of ANSYS CFD
Ryzhkov V.V., Morozov I.I.
Analysis of low-thrust liquid rocket engines with a methane air pump unit
Ivanov A.I., Kositsin I.P., Borisov V.A.
Design of the gas turbine engine rotor wheel with ceramic blades
Sapronov D.V., Reznik S.V.
Seal designing in a structure of the cooling system in gas turbine engine
Vinogradov A.S., Myatlev A.S.
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.
Investigation of the possibility of the creation LREST by thrust 400 N with a baffle - centrifugal scheme of NT and NDMG mixing
Ageenko Y.I., Ilin I.V., Pegin I.V., Shalamov E.A.
Experience in the development of 11Д58MФ liquid rocket engines
Smolentsev A.A.
CFD-modeling of processes in a high-pressure oxidizer pump for the turbopump assembly of a liquid rocket engine
Zubanov V.M., Shabliy L.S.
The influence of booster design features on aicraft engine fan tonal noise
Khaletskiy Y.D., Korzhnev V.N., Pochkin Y.S.
Modelling of an ejector for turbine aeroengines for application in performance synthesis tools
Georgi J., Staudacher S., Falaleev S.V.
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.
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 thermoplastic hardening for restoration of fatigue durability of gas turbine disks
Vishnyakov M.A.
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.
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.
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.
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.
Conception of cycle life additivity and its application for determining the resource of aero engine disks
Tumanov N.V., Lavrentyeva M.A.
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.
Characteristics of the sampling instrument for measuring emissions of an aircraft gas turbine engine
Okhlobystin A.V., Lyubimov R.V., Sokolova N.N.
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.
Verification of energy efficiency of a low-thrust liquid-propellant engine with the deflector-centrifugal injecting pattern
Ageenko Y.I., Pegin I.V.
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.
Development liquid roket engine on component fuel liquefied natural gas and oxygen for reusable space launching systems
Efimochkin A.F., Khrisanfov S.P., Golubyatnik V.V., Kafarena P.V., Yeliseyev A.V.
Strength analysis of internal combustion engine elements by using ANSYS with taking into account heat processes in the combustion chamber
Biryuk V.V., Gorshkalev A.A., Kayukov S.S., Saigakov E.A.
Rotary isochoric combustion chamber of a gas turbine engine
Porshnev V.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.
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.
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.
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.
The combined fuel draining control system for liquid oxygen and liquid hydrogen upper stage
Ivanov V.P., Partola I.S.
Multi-purpose high-precision thermal vacuum testing bench and someresults of firing tests of non-hypergolic low-thrust rocket engines
Ryzhkov V.V., Verjasov Y.N., Galperin R.N., Gulyaev Y.I., Ivashin Y.S.
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.
The projecting of gas turbine engine composite blades
Ryzhov A.A., Galimkhanov B.K., Ryzhov N.A., Latypov R.K., Irgalin S.R.
Hard & soft complex for “Angara” family launch vehicles engine system development
Partola I.S.
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.
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.
Verification of a design model and evaluation of a technique of manufacturing aircraft engine composite parts on the basis of dynamic tests
Zinin A.V., Arkhipov A.N., Kholobtsev D.P., Ravikovich Y.A., Shevjakov A.O., Kholmanova M.A.
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.
Analysis of nonstationary thermal state of low-thrust liquid rocket engine with high-concentration hydrogen peroxide and kerosene propellant with film cooling
Vorobiev A.G., Borovik I.N., Ha S.
Examination of the theoretical possibility of creating a vernier electrorocket engine
Baigaliev B.E., Chernoglazova A.V., Tumakov E.A., Temnikova S.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.
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.
Test bench for investigation of thrusters intra-chamber working processes
Pervyshin A.N., Ryazanov A.I.
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.
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.
Procedure of validated CFD-modeling of a two-stage screw-centrifugal pump
Zubanov V.M., Shabliy L.S., Krivtsov A.V., Ivanov A.I., Kositsin I.P., Baturin N.V.
Construction of a promising face gas-dynamic seal of the aircraft engine
Bondarchuk P.V., Falaleev S.V.
Automated profiling of tool electrode in electrochemical pulse machining
Nekhoroshev M.V., Pronichev N.D., Smirnov G.V.
Improving the quality parameters of serial debug two spool mixed flow turbofan
Volik A.A., Gumerov K.S., Khabibullin R.Z., Khayrullin R.B.
Some results of experimental refining of a constant volume valve combustion chamber
Bogdanov V.I., Kuznetsov S.P.
Life of gas turbine engine components under corrosive exposure
Pivovarova M.V., Gladkiy I.L.
Computer-aided system of virtual gas turbine engine testing
Tkachenko A.Y., Rybakov V.N., Krupenich I.N., Ostapuk Y.A., Filinov E.P.
Spacecraft preset orbital parameters control by means of thrusters
Salmin V.V., Volotsuev V.V., Shikhanov S.V.
Identification and procedure of reducing periodic noise of internal combustion car engines using the active compensation method
Vasilyev A.V., Andreyev S.S., Butsayev I.V., Pimkin V.V.
Fluctuations of pressure in rail gas injection of engines with spark ignition
Shishkov V.A.
Vibrodiagnostics of turboprop engine gearbox wear
Sundukov A.Y., Sundukov Y.V., Plotnikov S.M.
Definition of overall limits internal-combustion engine using vector modeling
Kosenok B.B.
Development of improved performance electromagnetic valve for liquid rocket engine
Igolkin A.A., Chubenko T.A., Maksimov A.D.
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