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Title
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Development of a mathematical model of the internal structure of a granular heat accumulator for launching a mono-fuel gas generator
Zrelov V.A., Lykin A.Y.
Gas turbine engine designing on the basis of a unified gas generator
Rybakov V.N.
Vortex gas wind-driven power plant for supplying compressor stations with electrical energy
Biryuk V.V., Zubrilin I.A., Krasnorutskiy A.S.
Optimization features of the working process parameters of bypass engine on the basis of given gas generator
Rybakov V.N.
Problem formulation of bypass engine parameters optimization with a preselected gas generator
Kuzmichev V.S., Kulagin V.V., Tkachenko A.Y., Krupenich I.N., Rybakov V.N.
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.
The task of creating the bypass engines of various thrust levels using the given gas generator
Kocherov E.P., Kuzmichev V.S., Kulagin V.V., Fedorchenko D.G.
Simulation and research of factors affecting aerodynamic indices of the gas purification process
Usmanova R.R., Zhernakov V.S.
Mathematical modelling of the working process of a hot gas pressure feed system
Salich V.L.
Theory of gas turbine engine optimal gas generator
Grigoriev A.V., Kosmatov A.A., Rudakov О.A., Solovieva A.V.
Methods of increase of wear resistance and vibroakusticheskikh of parameters of knots of the friction of space equipment
Gromakovsky D.G., Kovshov A.G., Kotcherov E.P., Makaryants M.V.
Features of optimization of the versatile gas generator parameters and design for development of a broad power range line of the advanced gas turbine engines of different application
Sharova N.A.
Designing GTE on the basis of versatile gas generator small dimension
1 1., 1 1.
Development of the active gas generator for high altitude firing test benches
Salich V.L.
Estimating the efficiency of a bypass turbojet engine on the basis of a serial gas generator as a part of the power plant of a high-altitude unmanned aerial vehicle
Zinenkov Y.V., Lukovnikov A.V., Popov A.V., Nechaev V.N.
System of pressurization of the fuel tank of a launch vehicle using the heat of generator gas
Biryuk V.V., Smorodin A.V., Shepelev A.I., Onoprienko D.A.
1 - 16 of 16 Items

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