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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.

(Rus)

Influence of the turbine ignition, flame tube suspension and nozzles on the combustion chamber characteristics

Matveev S.G., Orlov M.Y., Zubrilin I.A.

(Rus)

Estimation of parameters of a pulse detonation engine (РDЕ)

Anakin A.T., Tsybizov Y.I.

(Rus)

Vol 14, No 2 (2015)

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.

(Rus)

Vol 18, No 2 (2019)

Theory of gas turbine engine optimal gas generator

Grigoriev A.V., Kosmatov A.A., Rudakov О.A., Solovieva A.V.

(Rus)

Development of pneumatic- type starting nozzles for a full-scale low emission combustion chamber

Vasilyev A.J., Blumkin P.I., Chelebyan O.G.

(Rus)

Vol 19, No 2 (2020)

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.

(Rus)

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.

(Rus)

Vol 18, No 1 (2019)

Theoretical and experimental studies of a gas stamping device with a piston pressure multiplier

Botashev A.Y., Bayramukov R.A.

(Rus)

Vol 15, No 4 (2016)

Characteristics of a fuel spray downstream the pressure atomizers under high pressure in the combustion chamber

Sviridenkov A.A., Tretyakov V.V.

(Rus)

Vol 10, No 5 (2011)

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.

(Rus)

Vol 10, No 5 (2011)

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.

(Rus)

Vol 13, No 5-2 (2014): Special Issue

Results of numerical modeling of two-phase liquid / gas flow on the basis of a simplifield model of oil chamber

Lisitcin A.N., Badernikov A.V., Pechenik E.V.

(Rus)

Vol 11, No 1 (2012)

Approximate correlative-spectral analysis of temperature patterns of combustion chambers

Prokhorov S.A., Ilinsky S.A., Aleksandrova T.G., Solovyova Y.V.

(Rus)

Vol 10, No 2 (2011)

Construction of a promising face gas-dynamic seal of the aircraft engine

Bondarchuk P.V., Falaleev S.V.

(Rus)

Vol 8, No 3-1 (2009): Special Issue

Analysis and ballistics project the gun tube system with a joined drive on chamber

Safronov A.I., Potapenko V.V.

(Rus)

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.

(Rus)

Vol 19, No 1 (2020)

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.

(Rus)

Analysis and ballistics design of a laboratory installation system a small calibre with a joined drive on chambers

Safronov A.I., Zorkin V.A., Potapenko V.V.

(Rus)

Vol 17, No 4 (2018)

Comparative analysis of fuel distribution downstream of the gas-dynamic flame holder with various methods of injection

Tretyakov V.V., Sviridenkov A.A.

(Rus)

Vol 15, No 4 (2016)

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.

(Rus)

Vol 10, No 5 (2011)

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.

(Rus)

Vol 14, No 2 (2015)

Experience of operational development of starting characteristics of the APU combustion chamber

Chechulin A.Y.

(Rus)

Vol 13, No 5-1 (2014): Special Issue

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.

(Rus)

Vol 11, No 5-1 (2012): Special Issue

Optimization of design diffuser of GTE combustion chamber with using CAE-systems

Orlov M.Y., Matveev S.S., Zinkovskiy V.S.

(Rus)

Vol 10, No 2 (2011)

Some results of experimental refining of a constant volume valve combustion chamber

Bogdanov V.I., Kuznetsov S.P.

(Rus)

Vol 8, No 3-1 (2009): Special Issue

Agency of members of the pulse detonation engine on thrust characteristics

Porshnev V.A.

(Rus)

Homogeneous burners of two-staged combustion chambers

Grechishnikov O.V., Ostapets I.I., Roslyakov A.D., Tsybizov Y.I.

(Rus)

Vol 21, No 1 (2022)

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.

(Rus)

Vol 10, No 3-4 (2011): Special Issue

Working process of gaseous fuel metallizator

Pervyshin A.N., Ryazanov A.I.

(Rus)

Testing of combined air-rocket engine mak-up with pulsing combustion chamber

Solodovnikov A.V., Vishegorodcev E.N., Golubyatnik V.V.

(Rus)

Vol 17, No 4 (2018)

Experimental research on the development of an “oxygen (gas) + kerosene” – fueled thruster

Salich V.L.

(Rus)

Vol 15, No 3 (2016)

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.

(Rus)

Vol 10, No 5 (2011)

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.

(Rus)

Vol 14, No 2 (2015)

Fuel spraying and mixing in a simulated combustion chamber in the presence of air flow precession

Sviridenkov A.A., Tretyakov V.V.

(Rus)

Vol 11, No 5-2 (2012): Special Issue

Problems and solutions of using computer technologies in designing of combustion chambers GTE

Matveev S.G., Orlov M.Y., Zubrilin I.A.

(Rus)

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.

(Rus)

Vol 9, No 1 (2010)

Peculiarities of gas temperature field formation at the exit of small-sized gas turbine engine combustion chambers

1 1., 1 1., 1 1.

(Rus)

Vol 8, No 2 (2009)

Rotor blade compressor working process analysis

Dovgyallo A.I., Kolomin I.V.

(Rus)

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.

(Rus)

Vol 20, No 4 (2021)

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.

(Rus)

Vol 10, No 3-4 (2011): Special Issue

Test bench for investigation of thrusters intra-chamber working processes

Pervyshin A.N., Ryazanov A.I.

(Rus)

The numerical modelling of processes in combustion chambers of low thrust rocket engines

Salich V.L.

(Rus)

Vol 17, No 2 (2018)

Biological module “BiNOM” for cubesats of the SamSat family

Zakharov V.P., Konyukhov V.N., Bakhtinov P.I., Molchkov E.V., Kornilin D.V., Konovalov S.G.

(Rus)

Vol 15, No 3 (2016)

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.

(Rus)

Vol 10, No 5 (2011)

Development and research of a low-toxic combustion chamber of a stationary GTE

Markushin A.N., Merkushin V.K., Baklanov A.V.

(Rus)

Vol 11, No 3-3 (2012): Special Issue

Simulating of Roots compressor

Belov G.O., Ermilov M.A., Kryuchkov A.N.

(Rus)

Thermal state of combustor can elements

Grechishnikov O.V., Ostapets I.I., Roslyakov A.D., Tsybizov Y.I.

(Rus)

Experimental determination of the side forces acting on the combustion chamber in the altitude chamber at startup

, , , ,

(Rus)

Vol 7, No 3 (2008): Special Issue

A model of motion of monodispersible gas-liquid stream is in transzvukovoy of part of rocket chamber

Еpishchenko S.V., Pervishin A.N.

(Rus)

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.

(Rus)

Vol 20, No 3 (2021)

Introduction to the problem of calculating the parameters of the mixing chamber of an afterburning bypass engine

Karev O.D.

(Rus)

Vol 10, No 3-4 (2011): Special Issue

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.

(Rus)

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.

(Rus)

Vol 16, No 4 (2017)

Development of a new collector device for gas turbine engine afterburner

Teslya D.N., Mayatsky S.A., Grasko T.V.

(Rus)

Vol 14, No 4 (2015)

Investigation of the causes of crack origination in the inner casing of NK-86 gas turbine engine combustion chamber

Kocherova Е.Е.

(Rus)

Vol 10, No 5 (2011)

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.

(Rus)

Vol 14, No 2 (2015)

Experimental research of internal heat transfer in the vortex heat generator

Zhornik M.N., Piralishvili S.A., Mogileva K.A.

(Rus)

Vol 11, No 3-1 (2012): Special Issue

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.

(Rus)

Peculiarities of application of biofuel mixture in combustion chambers of modern gas turbine engines

Vasilyev A.J., Medvedev R.S., Chelebyan O.G.

(Rus)

Experimental development of the LRE with CCCM nozzle’s extension

(Rus)

Vol 12, No 2 (2013)

Agreement between criterial equations of heat transfer in the process of cooling aluminium ingots and experimental data

Gorshenin A.S., Krivosheev V.E.

(Rus)

Test benches for researching the processes and operational development of low emission gas turbine engine combustion chambers

Markushin A.N., Baklanov A.V.

(Rus)

Vol 20, No 3 (2021)

Experimental studies of the components of high-frequency ion engine RD0310

Kazbanov A.A., Dronov P.A., Spivak O.O., Derkachev A.B.

(Rus)

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.

(Rus)

Vol 16, No 3 (2017)

Modeling external thermal influence of infrared radiation sources during tests of rocket and space equipment in VK-600/300

Dobritsa D.B., Ushakova A.A., Shabarchin A.F., Yashchenko B.Y.

(Rus)

Vol 10, No 5 (2011)

Modeling of fuel vaporization and mixing processes in combustion chamber

Tretiyakov V.V.

(Rus)

Vol 10, No 5 (2011)

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.

(Rus)

Vol 13, No 5-4 (2014): Special Issue

Experience in the development of 11Д58MФ liquid rocket engines

Smolentsev A.A.

(Rus)

Vol 11, No 3-1 (2012): Special Issue

Calculation methodology of intermittent burning chamber main parameters

Solodovnikov A.V., Vishegorodcev E.N., Golubyatnik V.V.

(Rus)

Development of advanced low thrust rocket engines with ecologically friendly propellants

1 1., 1 1., 1 1.

(Rus)

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.

(Rus)

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.

(Rus)

Vol 20, No 3 (2021)

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.

(Rus)

Physical workflow model in the combustion chamber LREST with a jet-centrifugal jets on hypergolic propellants

Silyutin M.V., Shustov S.A.

(Rus)

Vol 18, No 1 (2019)

Development of blend composition of aviation kerosene surrogate for the simulation of workflow of gas turbine engine combustion chamber

Matveev S.G.

(Rus)

Vol 16, No 2 (2017)

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.

(Rus)

Vol 10, No 5 (2011)

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.

(Rus)

Vol 10, No 5 (2011)

Research of the process of cleaning gas from mechanical impurities in a direct flow centrifugal separator

Glebov G.A., Hazbulatov A.I.

(Rus)

Vol 13, No 5-4 (2014): Special Issue

Modeling of intrachamber processes in an oxygen-hydrogen thruster

Vaulin S.D., Salich V.L.

(Rus)

Vol 14, No 3 (2014)

Universal approach to the description of working medium chambers for simulating hydraulic and pneumatic systems

Timofeyev Y.M., Khalatov E.M.

(Rus)

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.

(Rus)

Manipulate pulsed detonation engine

1 1., 1 1.

(Rus)

Simulation of drop coagulations in swirled time dependent streams with reference to gas turbine engine combustion chambers

Sviridenkov A.A., Tretyakov V.V.

(Rus)

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.

(Rus)

Vol 20, No 2 (2021)

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.

(Rus)

Analisys of experimental combustion chambers fire tests for LRE with cooling by liquid oxigen for "DM" type booster

Smolentsev A.A., Strizhenko P.P.

(Rus)

Vol 18, No 1 (2019)

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.

(Rus)

Vol 15, No 4 (2016)

Unstady heat-mass-transfer and fuel distributions in flows downstream the gas-dynamic flame holder

Tretyakov V.V., Sviridenkov A.A.

(Rus)

Vol 10, No 5 (2011)

Research of toxic substances emission during water injection into a combustion chamber

Mingazov B.G., Mukhametgaliev T.H.

(Rus)

Vol 10, No 5 (2011)

Experimental investigations of fluid atomization by model frontal devices of combustion chambers

Vasilyev A.Y., Sviridenkov A.A., Tretyakov V.V.

(Rus)

Vol 13, No 5-4 (2014): Special Issue

Development of thruster chamber operating on oxygen-hydrogen fuel

Salich V.L.

(Rus)

Vol 11, No 2 (2012)

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.

(Rus)

Vol 10, No 3-1 (2011): Special Issue

The influence of burner design on the characteristics of the combustion chamber with gaseous fuels

Markushin A.N., Baklanov A.V., Tsyganov N.E.

(Rus)

Vol 8, No 3-1 (2009): Special Issue

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.

(Rus)

The influence of engineering changes on NOx emission in a gas-turbine endine combustion chamber

Mingazov B.G., Baklanov A.V.

(Rus)