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Optimization of operation mode and design parameters of a finely-dispersed metallic liquid-alloy generator
Egorychev V.S., Ryazanov A.I., Khaimovich A.I.
Study of the efficiency of the application of gas dynamic stabilization of the flame in a current engine
Belonozhkin V.V., Teslya D.N.
Theory of gas turbine engine optimal gas generator
Grigoriev A.V., Kosmatov A.A., Rudakov О.A., Solovieva A.V.
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.
Research of toxic substances emission during water injection into a combustion chamber
Mingazov B.G., Mukhametgaliev T.H.
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.
Development of pneumatic- type starting nozzles for a full-scale low emission combustion chamber
Vasilyev A.J., Blumkin P.I., Chelebyan O.G.
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.
Testing of combined air-rocket engine mak-up with pulsing combustion chamber
Solodovnikov A.V., Vishegorodcev E.N., Golubyatnik V.V.
Optimization of fuel distribution in the afterburner of a gas turbine engine
Nelyubin V.R.
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.
Development and research of a low-toxic combustion chamber of a stationary GTE
Markushin A.N., Merkushin V.K., Baklanov 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.
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.
Peculiarities of gas temperature field formation at the exit of small-sized gas turbine engine combustion chambers
1 1., 1 1., 1 1.
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.
Mathematical model for calculating pressure in a pulsating combustion chamber
Solodovnikov A.V., Odentsov D.A., Kravtsov E.V., Golubyatnik V.V., Shcheblykin D.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.
The numerical modelling of processes in combustion chambers of low thrust rocket engines
Salich V.L.
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.
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.
Experience in the development of 11Д58MФ liquid rocket engines
Smolentsev A.A.
3d calculation of a multiport low-emission combustor cooling system
Moreva I.S., Vasilyuk D.K., Kirichenko R.Y.
Test benches for researching the processes and operational development of low emission gas turbine engine combustion chambers
Markushin A.N., Baklanov A.V.
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.
Development of a new collector device for gas turbine engine afterburner
Teslya D.N., Mayatsky S.A., Grasko T.V.
Investigation of the gas turbine engine combustion chamber workflow
Markushin A.N., Baklanov 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.
Modeling of intrachamber processes in an oxygen-hydrogen thruster
Vaulin S.D., Salich V.L.
Peculiarities of application of biofuel mixture in combustion chambers of modern gas turbine engines
Vasilyev A.J., Medvedev R.S., Chelebyan O.G.
Study of flow characteristics in straight-flow combustion chamber with sudden expansion
Egorov A.G., Zotkin V.I., Ivanin S.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.
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.
Development of blend composition of aviation kerosene surrogate for the simulation of workflow of gas turbine engine combustion chamber
Matveev S.G.
Development of a low-emission bifuel combustion chamber
Bubentsov A.V., Vasiluk D.K., Golubev P.A., Kirichenko R.E., Tashkinov V.A., Shoshin V.B.
Development of advanced low thrust rocket engines with ecologically friendly propellants
1 1., 1 1., 1 1.
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.
Analisys of experimental combustion chambers fire tests for LRE with cooling by liquid oxigen for "DM" type booster
Smolentsev A.A., Strizhenko P.P.
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.
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.
Modeling of fuel vaporization and mixing processes in combustion chamber
Tretiyakov V.V.
Experimental investigations of fluid atomization by model frontal devices of combustion chambers
Vasilyev A.Y., Sviridenkov A.A., Tretyakov V.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.
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.
Manipulate pulsed detonation engine
1 1., 1 1.
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.
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.
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.
Theoretical and experimental studies of a gas stamping device with a piston pressure multiplier
Botashev A.Y., Bayramukov R.A.
Unstady heat-mass-transfer and fuel distributions in flows downstream the gas-dynamic flame holder
Tretyakov V.V., Sviridenkov A.A.
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.
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.
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.
Numerical investigation multifuel combustion gas turbine combustion chamber module
Malygina M.V.
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.
Simulation of drop coagulations in swirled time dependent streams with reference to gas turbine engine combustion chambers
Sviridenkov A.A., Tretyakov V.V.
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.
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.
Comparative analysis of fuel distribution downstream of the gas-dynamic flame holder with various methods of injection
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.
Fuel spraying and mixing in a simulated combustion chamber in the presence of air flow precession
Sviridenkov A.A., Tretyakov V.V.
Combined calculation of gas generators of small GTE in package ANSYS CFX
Matveev S.G., Orlov M.Y., Matveev S.S., Zinkovskii V.S., Krivtsov A.V.
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.
The influence of burner design on the characteristics of the combustion chamber with gaseous fuels
Markushin A.N., Baklanov A.V., Tsyganov N.E.
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.
Test case of 3d unsteady swirling flows modeling using commercial and in-house codes
Nazukin V.A., Avgustinovich V.G., Thornber B., Aguado Lopez P., Tsatiashvili V.V., Koromyslov E.V.
Сalculation of characteristics of atomization of liquid supplied at an angle to the flow direction and justification of adjusting the angle of the nozzle inclination relative to the gas flow
Teslya D.N., Mityaev S.V., Drobyshev P.A.
Thermal physics of hydrogen-oxygen combuster chambers for high-temperature turbines combined-cycle power plant
Guryanov A.I., Piralishvili G.S., Vereschagin I.M.
Experimental research on the development of an “oxygen (gas) + kerosene” – fueled thruster
Salich V.L.
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.
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.
Approximate correlative-spectral analysis of temperature patterns of combustion chambers
Prokhorov S.A., Ilinsky S.A., Aleksandrova T.G., Solovyova Y.V.
Some results of experimental refining of a constant volume valve combustion chamber
Bogdanov V.I., Kuznetsov S.P.
The influence of engineering changes on NOx emission in a gas-turbine endine combustion chamber
Mingazov B.G., Baklanov A.V.
1 - 74 of 74 Items

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