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Title
Authors
Peculiarities of starting a spark-ignition gas fuel internal combustion engine
Shishkov V.A.
Experimental and numerical investigation of the combustion process in vortex gas burner
Yevdokimov O.A.
Investigation of transformation of intermediate products of liquid-phase interaction propellant at the onset of combustion for rocket engine
Nigodjuk V.E., Sulinov A.V.
Using the energy of gas differential pressure in electromagnetic injectors for improved breathing of spark-ignition internal combustion engine cylinders
Shishkov V.A.
The mixing efficiency of liquid droplet fuel and air flow in the frontal swirl devices
1 1., 1 1.
Operation of an electronic system of control for spark-ignition gas fuel internal combustion engines in ignition misses
Shishkov V.A.
On selection of automatic control system for crvogenic fuel gas turbine engine
Bukin V.A.
Cycle parameters of an internal combustion spark-ignition gas piston engine with an electronic control system
Shishkov V.A.
Definition of directions of developing methods, technical decisions and means of decreasing the technogenic influence on the environment for the omplementation on board of space launch vehicles
Shatrov Y.T., Baranov D.A., Trushlyakov V.I., Kudentsov V.Y.
Modeling direct fuel injection by a multipin nozzle into the ice combustion chamber using CAE/CAD-systems
Biryuk V.V., Kayukov S.S., Gorshkalev A.A., Uglanov D.A., Lysenko Y.D., Zvyagintsev V.A.
Features of start-up the engine of internal combustion with spark ignition on gas fuel
Shishkov V.A.
Technology of computational analysis of the working process parameters of low-thrust rocket engines running on gaseous oxygen-hydrogen fuel with the use of ANSYS CFD
Ryzhkov V.V., Morozov I.I.
Oxygen-hidrogen liquid rocket engine using turbo-pump developed for aviation hidrogen liquid two-spool turbo-jet
Ivanov A.I., Borisov V.A.
Quality indices of an internal combustion engine controlled by the discharge current channel
1 1., 1 1., 1 1.
Investigation of the kinetic properties of gas products of liquid-phase interaction hypergolic liquid rocket fuel
Nigodjuk V.E., Sulinov A.V.
Choosing the mixing pattern for oxygen-hydrogen low-thrust rocket engines
Ryzhkov V.V., Morozov I.I.
Determining the angle of advance of ignition when switching from petrol to gas depending on fuel mixture burning rate
Shishkov V.A.
Optoelectronic device for the control of hydrocarbon fuel cavitation treatment
1 1.
Method of design calculation jet-centrifugal gas-liquid duplex fuel nozzle with internal mixing
Egorychev V.S.
Analysis of low-thrust liquid rocket engines with a methane air pump unit
Ivanov A.I., Kositsin I.P., Borisov V.A.
Model of sedimentation of solid particles of heterogeneous materials
Polyanskov Y.V., Evseev A.N., Poroykov V.A.
Defining the specific impulse of mixed solid propellants
1 1., 1 1.
Method of design calculation gas-liquid jet duplex fuel nozzle with internal mixing
Egorychev V.S.
Experimental study of free-convection flame propagation
Yevdokimov O.A., Guryanov A.I.
Approaches to the evaluation of fuels for hypersonic engines
Sergeev S.M., Petrukhin N.V.
Mathematical model of small-thrust rocket engine with gaseous oxygen and hydrogen in pulse operation
1 1.
Improving the efficiency of the powerplant of an unmanned aerial vehicle through the use of cryogenic fuel
Kolesnikov A.S., Grasko T.V., Raznoschikov V.V.
Prospects and problems of movement and power plants in powder metal fuel
Egorov A.G., Tizilov A.S.
Estimation of mass-dimensional characteristics of a complex propulsion unit of earth remote sensing spacecraft
Kurenkov V.I., Kucherov A.S., Yakishik A.A.
Quasi one-dimensional model and calculation of processes in gas turbineengine combustion chambers given the heterogeneity of the combustible mixture, changes in mass, composition, temperature and stirring efficiency of the working body
Didenko A.A., Sokolov A.B.
Мethod of design calculation of centrifugal emulsive duplex fuel nozzle
1 1.
Сalculated analysis of the influence of operation and design factors on the parameters of oxygen-hydrogen low-thrust rocket engines
Ryzhkov V.V., Morozov I.I.
Possibility of use of passing gases in gasturbine engines created within the limits of conversion
Rosljakov A.D., Kocherov E.P., Tsibizov J.I.
Results of experimental studies of parameters of low-thrust rocket engines operating on gaseous oxygen-hydrogen fuel
Ageenko Y.I., Lapshin E.A., Morozov I.I., Pegin I.V., Ryzhkov V.V.
Algorithm of adaptation of an electronic control system of internal combustion engines to various chemical compositions of gas fuel
Shishkov V.A.
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.
1 - 36 of 36 Items

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