Issue
Title
Authors
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.
Influence of the turbine ignition, flame tube suspension and nozzles on the combustion chamber characteristics
Matveev S.G., Orlov M.Y., Zubrilin I.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.
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.
Development of pneumatic- type starting nozzles for a full-scale low emission combustion chamber
Vasilyev A.J., Blumkin P.I., Chelebyan O.G.
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.
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.
Simulation of drop coagulations in swirled time dependent streams with reference to gas turbine engine combustion chambers
Sviridenkov A.A., Tretyakov V.V.
Interconnection of propagation velocity and electrical conductivity of flame in ICEs
Ivashin P.V., Ramazanov M.P., Tverdokhlebov A.Y., Shaikin A.P., Yasnikov I.S.
Peculiarities of application of biofuel mixture in combustion chambers of modern gas turbine engines
Vasilyev A.J., Medvedev R.S., Chelebyan O.G.
The influence of engineering changes on NOx emission in a gas-turbine endine combustion chamber
Mingazov B.G., Baklanov A.V.
Theory of gas turbine engine optimal gas generator
Grigoriev A.V., Kosmatov A.A., Rudakov О.A., Solovieva A.V.
Experience of operational development of starting characteristics of the APU combustion chamber
Chechulin A.Y.
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.
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.
Homogeneous burners of two-staged combustion chambers
Grechishnikov O.V., Ostapets I.I., Roslyakov A.D., Tsybizov Y.I.
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.
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.
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.
Test benches for researching the processes and operational development of low emission gas turbine engine combustion chambers
Markushin A.N., Baklanov A.V.
The influence of burner design on the characteristics of the combustion chamber with gaseous fuels
Markushin A.N., Baklanov A.V., Tsyganov N.E.
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.
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.
Thermal state of combustor can elements
Grechishnikov O.V., Ostapets I.I., Roslyakov A.D., Tsybizov Y.I.
Experience in the development of 11Д58MФ liquid rocket engines
Smolentsev A.A.
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.
Development of blend composition of aviation kerosene surrogate for the simulation of workflow of gas turbine engine combustion chamber
Matveev S.G.
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.
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.
Peculiarities of gas temperature field formation at the exit of small-sized gas turbine engine combustion chambers
1 1., 1 1., 1 1.
Modeling of intrachamber processes in an oxygen-hydrogen thruster
Vaulin S.D., Salich V.L.
Fuel spraying and mixing in a simulated combustion chamber in the presence of air flow precession
Sviridenkov A.A., Tretyakov V.V.
Influence of the burner form on the combustion chamber outlet temperature field ripple for different modes of operation of gas turbine engines
Markushin A.N., Baklanov A.V.
Some results of experimental refining of a constant volume valve combustion chamber
Bogdanov V.I., Kuznetsov S.P.
Problems and solutions of using computer technologies in designing of combustion chambers GTE
Matveev S.G., Orlov M.Y., Zubrilin I.A.
Research of toxic substances emission during water injection into a combustion chamber
Mingazov B.G., Mukhametgaliev T.H.
Theoretical and experimental studies of a gas stamping device with a piston pressure multiplier
Botashev A.Y., Bayramukov R.A.
New technologies implemented in the design of a low-emission combustion chamber of a gas-turbine unit
Fedorchenko D.G., Tsybizov Y.I., Tyulkin D.D., Vorotyntsev I.E., Zherelov D.A., Dulov A.S., Smelov V.G., Sotov A.V., Agapovichev A.V.
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.
Comparative analysis of fuel distribution downstream of the gas-dynamic flame holder with various methods of injection
Tretyakov V.V., Sviridenkov A.A.
Experimental research on the development of an “oxygen (gas) + kerosene” – fueled thruster
Salich V.L.
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 new collector device for gas turbine engine afterburner
Teslya D.N., Mayatsky S.A., Grasko T.V.
Formulas of reducing engine environmental performance and combustion characteristics to standard atmospheric conditions
Grigoriev A.V., Kosmatov A.A., Rudakov O.A., Solovieva A.V.
Unstady heat-mass-transfer and fuel distributions in flows downstream the gas-dynamic flame holder
Tretyakov V.V., Sviridenkov A.A.
Characteristics of a fuel spray downstream the pressure atomizers under high pressure in the combustion chamber
Sviridenkov A.A., Tretyakov V.V.
Approximate correlative-spectral analysis of temperature patterns of combustion chambers
Prokhorov S.A., Ilinsky S.A., Aleksandrova T.G., Solovyova Y.V.
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.
Analisys of experimental combustion chambers fire tests for LRE with cooling by liquid oxigen for "DM" type booster
Smolentsev A.A., Strizhenko P.P.
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.
Specifying the dimensions of the reverse current area of a 3-D gas-turbine engine combustion chamber model using the ANSYS FLUENT software
Biryuk V.V., Orlov M.Y., Zubrilin I.A., Sinegovskiy Y.A., Krivtsov A.V.
Optimization of design diffuser of GTE combustion chamber with using CAE-systems
Orlov M.Y., Matveev S.S., Zinkovskiy V.S.
Modeling of propane combustion processes in case of converting a GTE combustion chamber to gaseous fuel
Matveev S.G., Lanskiy A.M., Orlov M.Y., Abrashkin V.Y., Dmitriev D.N., Zubrilin I.A., Semenov A.V.
Tests of the low emission combustion chambers compartment with pressure and pressure–air assist atomizers
Maslov V.P., Mashinistova N.P., Sviridenkov A.A., Jagodkin V.I.
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.
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.
Investigation of the causes of crack origination in the inner casing of NK-86 gas turbine engine combustion chamber
Kocherova Е.Е.
Testing of combined air-rocket engine mak-up with pulsing combustion chamber
Solodovnikov A.V., Vishegorodcev E.N., Golubyatnik V.V.
Modeling of fuel vaporization and mixing processes in combustion chamber
Tretiyakov V.V.
The numerical modelling of processes in combustion chambers of low thrust rocket engines
Salich V.L.
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.
Methodology of optimization of parameter of matching the combustion chamber and turbine joint operation
Grigoriev A.V., Golubchikov P.P., Ilushin M.Y., Rudakov O.A., Solovieva A.V.
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.
Development of advanced low thrust rocket engines with ecologically friendly propellants
1 1., 1 1., 1 1.
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.
Experimental investigations of fluid atomization by model frontal devices of combustion chambers
Vasilyev A.Y., Sviridenkov A.A., Tretyakov V.V.
Manipulate pulsed detonation engine
1 1., 1 1.
Physical workflow model in the combustion chamber LREST with a jet-centrifugal jets on hypergolic propellants
Silyutin M.V., Shustov S.A.
Experimental development of the LRE with CCCM nozzle’s extension
,
1 - 69 of 69 Items

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