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Development of blend composition of aviation kerosene surrogate for the simulation of workflow of gas turbine engine combustion chamber
Matveev S.G.
The limits ofdistributionin aflamealuminum-air mixture
Tizilov A.S., Egorov A.G.
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.
Formation of microvortex gas flows in channels of a block catalyst with coplanar channels
Knysh Y.A., Tsibizov Y.I., Dmitriev D.N., Gorshkalev 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.
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.
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 swirling of a flow with axial countercurrent on the process of burning of hydrogenoxygen mix in the stream of water steam
Guryanov A.I., Vereshchagin I.M.
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.
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.
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.
Combustion of condensed substance in the electrostatic field
Zyryanov I.A., Pozolotin A.P.
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.
Defining the specific impulse of mixed solid propellants
1 1., 1 1.
Application of flame electro conductivity for combustion analysis in spark ignition ICE
Ivashin P.V.
ASMTurbC method of autonomous statistical modeling of diffusion turbulent combustion and the results of its testing
Nuzhnov Y.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.
Manipulate pulsed detonation engine
1 1., 1 1.
Experimental and numerical investigation of the combustion process in vortex gas burner
Yevdokimov O.A.
Statistical physics and cycles of operation of heat engines
Mikheenkov E.L.
Approaches to the evaluation of fuels for hypersonic engines
Sergeev S.M., Petrukhin N.V.
Pressure-gain combustion and its potential for gas turbine engine enhancement
Lutoschkin E.V., Rose M.G., Staudacher S.
Improving the efficiency of diesel engines by means of electroprocessing of fuel
Kozmenkov I.N., Nosyrev D.Y.
Experimental study of free-convection flame propagation
Yevdokimov O.A., Guryanov A.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.
Combustion of polymers in the electrostatic field
Reshetnikov S.M., Pozolotin A.P., Zyryanov I.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.
Formation in the channels of the block catalyst the micro vortex gas flows with intense twist
Knysh Y.A., Zibizov Y.I., Dmitriev D.N., Gorshkalev A.A.
3d calculation of a multiport low-emission combustor cooling system
Moreva I.S., Vasilyuk D.K., Kirichenko R.Y.
The influence of engineering changes on NOx emission in a gas-turbine endine combustion chamber
Mingazov B.G., Baklanov A.V.
1 - 30 of 30 Items

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