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Determination of completeness of combustion, temperature and emission characteristics in a swirl flow based on the theory of turbulent combustion
Aleksandrov Y.B., Mingazov B.G.
Optimization of operation mode and design parameters of a finely-dispersed metallic liquid-alloy generator
Egorychev V.S., Ryazanov A.I., Khaimovich A.I.
Research of toxic substances emission during water injection into a combustion chamber
Mingazov B.G., Mukhametgaliev T.H.
Design and development of combustion chambers for gas turbine engines based on calculations of various levels of complexity
Aleksandrov Y.B., Nguyen T.D., Mingazov B.G.
Experimental method for evaluating the balance of high-speed small-sized internal combustion engines
Rekadze P.D., Sychugov S.Y., Melentiev V.S., Rodionov L.V.
Energy sources in heat engine cycles
Mikheyenkov E.L.
Experience of operational development of starting characteristics of the APU combustion chamber
Chechulin A.Y.
Specific features of pressure pulsation control in combustion chambers of land based gas turbine units
Skiba D.V., Maksimov D.A., Kashapov R.S., Kharisov T.S.
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 methodology for calculating the working process of a small-size two-stroke internal combustion engine
Biryuk V.V., Gorshkalev A.A., Zakharov M.O., Larin V.L.
Experimental and numerical investigation of the combustion process in vortex gas burner
Yevdokimov O.A.
Increasing the efficiency and stability of fuel supply to the combustion chamber of a liquid rocket engine by spray nozzles
Ageenko Y.I., Bubnova A.S.
Statistical physics and cycles of operation of heat engines
Mikheenkov E.L.
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.
Applying the possibilities of Microsoft Excel for solving problems of fuel burning thermodynamics
Mikheenkov E.L., Nekrasova S.O., Ramzaeva E.A.
Determination of thermal state and modification of the flame tube cooling system with the help of three-dimensional modeling methods
Matveev S.G., Anisimov V.M., Zubrilin I.A., Kolomzarov O.V., Mironov N.S.
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.
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.
Numerical investigation multifuel combustion gas turbine combustion chamber module
Malygina M.V.
Common properties of hydrocarbon combustion products and Brayton cycle
Mikheenkov E.L.
Peculiarities of gas temperature field formation at the exit of small-sized gas turbine engine combustion chambers
1 1., 1 1., 1 1.
Effect of non-uniform compressor flow parameters on the characteristics of a gas turbine engine combustion chamber
Matveev S.G., Orlov M.Y., Zubrilin I.A., Matveev S.S., Tsybizov Y.I.
Theory of gas turbine engine optimal gas generator
Grigoriev A.V., Kosmatov A.A., Rudakov О.A., Solovieva A.V.
Indirect determination of the presence of vibration combustion in combustion chambers of turbine engines by a three-channel sensor for measuring movement
Limanova N.I., Yudin P.Y., Limanov I.A.
Multisprayer low-emission combustion chamber of modern turbojet engines – N. D. Kuznetsov’s creative heritage
Bantikov D.Y., Vasilyev V.I., Lavrov V.N., Tsibisov Y.I., Matveev S.G., Orlov M.Y., Zubrilin I.A.
Influence of the turbine ignition, flame tube suspension and nozzles on the combustion chamber characteristics
Matveev S.G., Orlov M.Y., Zubrilin I.A.
Development of blend composition of aviation kerosene surrogate for the simulation of workflow of gas turbine engine combustion chamber
Matveev S.G.
Characteristics of a fuel spray downstream the pressure atomizers under high pressure in the combustion chamber
Sviridenkov A.A., Tretyakov V.V.
Modeling of fuel vaporization and mixing processes in combustion chamber
Tretiyakov V.V.
Increasing the capacity of engine intake system
Kozin A.M., Rusakov M.M.
Experience in the development of 11Д58MФ liquid rocket engines
Smolentsev A.A.
The limits ofdistributionin aflamealuminum-air mixture
Tizilov A.S., Egorov A.G.
Approximate correlative-spectral analysis of temperature patterns of combustion chambers
Prokhorov S.A., Ilinsky S.A., Aleksandrova T.G., Solovyova Y.V.
Thermal state of combustor can elements
Grechishnikov O.V., Ostapets I.I., Roslyakov A.D., Tsybizov Y.I.
The influence of burner design on the characteristics of the combustion chamber with gaseous fuels
Markushin A.N., Baklanov A.V., Tsyganov N.E.
Experimental development of the LRE with CCCM nozzle’s extension
,
Technical solutions of NOx decrease in traditional combustion chamber of GTE NK-16ST
Markushin A.N., Merkushin V.K., Byshin V.M., Baklanov A.V.
Development of a generalized model of heat-mass transfer between fuel drops and gas stream with reference to gas turbine engine combustion chambers
Tretyakov V.V., Sviridenkov A.A.
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.
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.
Aspects of the numerical method calculating thermogazodynamic lrest based on not perfect passing of workflows in the combustion chamber
Silyutin M.V., Shustov S.A.
Working out of the design of the chamber of combustion of engine NK-14ST-10 with modular torches
Kocherov E.P., Rosljakov A.D., Tsibizov J.I.
Method of calculating the thickness of the combustion chamber of a liquid rocket engine made with the use of innovative technologies and materials
Krivonogov A.V.
Analysis of combustion models applicability for designing combustion chamber with a large number of nozzles
Mingazov B.G., Yavkin V.B., Sabirzyanov A.N., Baklanov A.V.
Using an ionization probe removed from the sparking plug for the development of a two-zone ICE combustion model
Ivashin P.V., Rybakov M.P.
Fuel spraying and mixing in a simulated combustion chamber in the presence of air flow precession
Sviridenkov A.A., Tretyakov V.V.
Modeling of intrachamber processes in an oxygen-hydrogen thruster
Vaulin S.D., Salich V.L.
On plasma support of fuel burning in a combustion chamber of a gas-turbine facility
Bulaeva M.N., Kravchenko I.V., Riaby V.A., Tkachenko D.P.
Optimization of design diffuser of GTE combustion chamber with using CAE-systems
Orlov M.Y., Matveev S.S., Zinkovskiy V.S.
Peculiarities of application of biofuel mixture in combustion chambers of modern gas turbine engines
Vasilyev A.J., Medvedev R.S., Chelebyan O.G.
Analysis of nonstationary thermal state of a low-thrust liquid rocket engine taking into account injection, evaporation and combustion of liquid fuel droplets
Vorobiev A.G., Borovik I.N., Ha S.
Development of advanced low thrust rocket engines with ecologically friendly propellants
1 1., 1 1., 1 1.
Modeling of the heat exchange processes
Limanova N.I., Mamzin E.A., Matveev S.G.
Simulation of drop coagulations in swirled time dependent streams with reference to gas turbine engine combustion chambers
Sviridenkov A.A., Tretyakov V.V.
Analyzing the quality of preparing fuel-air mixture and its influence on NOx in a low emission gas turbine engine combustion chamber
Markushin A.N., Baklanov A.V.
Homogeneous burners of two-staged combustion chambers
Grechishnikov O.V., Ostapets I.I., Roslyakov A.D., Tsybizov Y.I.
Features of start-up the engine of internal combustion with spark ignition on gas fuel
Shishkov V.A.
Theoretical and experimental studies of a gas stamping device with a piston pressure multiplier
Botashev A.Y., Bayramukov R.A.
Method of transient simulation of combustion processes in a low-thrust rocket engine operating on gaseous hydrogen and oxygen
Zubanov V.M., Shabliy L.S., Stepanov D.V.
Combustion of condensed substance in the electrostatic field
Zyryanov I.A., Pozolotin A.P.
ASMTurbC method of autonomous statistical modeling of diffusion turbulent combustion and the results of its testing
Nuzhnov Y.V.
Investigation of transformation of intermediate products of liquid-phase interaction propellant at the onset of combustion for rocket engine
Nigodjuk V.E., Sulinov A.V.
Interaction of exhaust jets of rocker propulsions on various propellants with atmosphere for estimation of ecological safety of firing of rockets and launchers
Zavelevich F.S., Ushakov N.N.
Approaches to the evaluation of fuels for hypersonic engines
Sergeev S.M., Petrukhin N.V.
Development of pneumatic- type starting nozzles for a full-scale low emission combustion chamber
Vasilyev A.J., Blumkin P.I., Chelebyan O.G.
Some results of experimental refining of a constant volume valve combustion chamber
Bogdanov V.I., Kuznetsov S.P.
Manipulate pulsed detonation engine
1 1., 1 1.
Pressure-gain combustion and its potential for gas turbine engine enhancement
Lutoschkin E.V., Rose M.G., Staudacher S.
Combustion of polymers in the electrostatic field
Reshetnikov S.M., Pozolotin A.P., Zyryanov I.A.
Test benches for researching the processes and operational development of low emission gas turbine engine combustion chambers
Markushin A.N., Baklanov A.V.
Method of reduced fuel characteristics and parameters of the operating cycles of heat engines
Anastaseev V.V., Belozertsev S.V., Mikheenkov E.L., Nekrasova S.O.
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.
Improving the efficiency of diesel engines by means of electroprocessing of fuel
Kozmenkov I.N., Nosyrev D.Y.
Comparative analysis of fuel distribution downstream of the gas-dynamic flame holder with various methods of injection
Tretyakov V.V., Sviridenkov A.A.
Efficiency of aft diffusers in vacuum systems of test benches for high-altitude firing tests of low-thrust liquid rocket engines
Galperin R.N., Gulyaev Y.I., Ivashin Y.S., Nigodjuk V.E., Ryzhkov V.V., Sulinov A.V.
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.
Investigation of thermal explosion in a pseudoliquid fuel
Yegorov A.G., Safronov A.I., Tizilov A.S., Ivanin S.V.
Cycle parameters of an internal combustion spark-ignition gas piston engine with an electronic control system
Shishkov V.A.
Mathematical model and peculiarities of operating mobile robots with hybrid drives
Ilyukhin Y.V., Tatarintseva A.V.
Emission characteristics and temperature non-uniformity at the outlet of the gas turbine engine combustion chamber
Sabirzyanov A.N., Yavkin V.B., Alexandrov Y.B., Markushin A.N., Baklanov A.V.
Algorithm of adaptation of an electronic control system of internal combustion engines to various chemical compositions of gas fuel
Shishkov V.A.
The simplification of heat engines thermodynamics calculation with using of idaeal gas’ model
1 1., 1 1.
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.
Mathematical model for calculating radial non-uniformity of the gas temperature field at the exit of small gas turbine engine combustion chambers
Lukachev S.V., Abrashkin V.Y., Lansky A.M., Matveev S.G.
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.
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.
Testing of combined air-rocket engine mak-up with pulsing combustion chamber
Solodovnikov A.V., Vishegorodcev E.N., Golubyatnik V.V.
Experimental research on the development of an “oxygen (gas) + kerosene” – fueled thruster
Salich V.L.
Using the phenomenon of electrical conduction of flame of non-homogeneous air-fuel mixture in design and development of combustion chamber
Shajkin A.P., Ivashin P.V., Galiev I.R., Derjachev A.D., Tverdohljobov A.J.
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.
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.
Problems and solutions of using computer technologies in designing of combustion chambers GTE
Matveev S.G., Orlov M.Y., Zubrilin I.A.
Determining the angle of advance of ignition when switching from petrol to gas depending on fuel mixture burning rate
Shishkov V.A.
3d calculation of a multiport low-emission combustor cooling system
Moreva I.S., Vasilyuk D.K., Kirichenko R.Y.
Hanges in volume combustion and concentration of nitrogen oxides in the exhaust gases gasoline engine
Kolomiets P.V.
Using the energy of gas differential pressure in electromagnetic injectors for improved breathing of spark-ignition internal combustion engine cylinders
Shishkov V.A.
The story of invention and development of supercharge units of internal combustion engines
1 1., 1 1., 1 1.
Model of varigrained particle stream moving by hypersonic combustion materials investigation
Bulanova E.A., Pervishin A.N.
The influence of engineering changes on NOx emission in a gas-turbine endine combustion chamber
Mingazov B.G., Baklanov A.V.
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.
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