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Title
Authors
Method of design calculation jet-centrifugal gas-liquid duplex fuel nozzle with internal mixing
Egorychev V.S.
Method of design calculation gas-liquid jet duplex fuel nozzle with internal mixing
Egorychev V.S.
Мethod of design calculation of centrifugal emulsive duplex fuel nozzle
1 1.
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.
Influence of pad geometry and method of oil supply on the thermal state of GTE rotor tilting-pad journal bearing
Parovay E.F.
Verification of energy efficiency of a low-thrust liquid-propellant engine with the deflector-centrifugal injecting pattern
Ageenko Y.I., Pegin I.V.
Mixing processe research in 10…15 N thrusters
Salich V.L., Semkin E.V.
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.
Research of liquid outflow from low-emission swirl injectors of a low-thrust liquid rocket engine
Semkin Y.V.
Development of pneumatic- type starting nozzles for a full-scale low emission combustion chamber
Vasilyev A.J., Blumkin P.I., Chelebyan O.G.
Characteristics of a fuel spray downstream the pressure atomizers under high pressure in the combustion chamber
Sviridenkov A.A., Tretyakov V.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.
Effect of coagulation of drops on fuel spray characteristics behind atomizers
1 1., 1 1.
Design and investigation of a pneumatic atomizer as applied to a low emission combustion chamber of a promising gas-turbine engine
Vasilyev A.Y., Chelebyan O.G., Yagodkin V.I.
The oretical substantiation of the constructive scheme of the air-gas tract rinsing device for GTE
Silaev B.M., Mal’tsev E.N.
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.
Experimental investigations of fluid atomization by model frontal devices of combustion chambers
Vasilyev A.Y., Sviridenkov A.A., Tretyakov V.V.
Research of the influence of design parameters of a 400 N-thrust low-thrust liquid rocket engine on its energy efficiency
Ageenko Y.I., Ilyin R.V., Pegin I.V.
1 - 18 of 18 Items

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