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Resistance of products made of steel 20GL to sulfide stress corrosion cracking
Blazhnov N.M., Borisenkova E.A., Khardin M.V.
On selection of automatic control system for crvogenic fuel gas turbine engine
Bukin V.A.
Development of turbopump unit design for hydrogen liquid-propellant rocket engines without generators developed at the design bureau of chemical automation
Dmitrenko A.I., Ivanov A.V., Rachuk V.S.
Methods of modeling the work process of hydrogen screw-centrifugal pumps using ANSYS CFD
Sulinov A.V., Shabliy L.S., Zubanov V.M.
Mathematical model of small-thrust rocket engine with gaseous oxygen and hydrogen in pulse operation
1 1.
Research of flame distribution speed, width of the zone and intensity of chemical reactions of combustion in the spark-ignition engine
Bobrovskiy I.N., Shaykin A.P., Brizgalov A.A., Sukhov S.A.
Hydrogenium saturation research for finishing pulsed electrochemical machining of titan alloy (BT9) TJ blades
Smirnov G.V.
Modeling of intrachamber processes in an oxygen-hydrogen thruster
Vaulin S.D., Salich V.L.
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.
Development of thruster chamber operating on oxygen-hydrogen fuel
Salich V.L.
Modelling system of cooling nozzle-sprayer hydrogen steam generator
Lazarenko I.N., Prigozhin A.A., Shmatov D.P.
Research of the influence of electron beam welding of titanium alloys on hydrogen distribution in the weld
Muravyev V.I., Bakhmatov P.V., Grigorev V.V., Shakirova O.G., Iskhakov S.A.
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.
Thermal physics of hydrogen-oxygen combuster chambers for high-temperature turbines combined-cycle power plant
Guryanov A.I., Piralishvili G.S., Vereschagin I.M.
Analysis of nonstationary thermal state of low-thrust liquid rocket engine with high-concentration hydrogen peroxide and kerosene propellant with film cooling
Vorobiev A.G., Borovik I.N., Ha S.
1 - 15 of 15 Items

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