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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.
Calculation of optimum transfers from high-elliptic orbits to geostationary orbits using a stationary plasma engine
Kvetkin A.A., Kolesov A.V.
Identification of a gas turbine engine mathematical model by the ressults of testing
Botchkaryov S.K., Dmitriyev A.Y.
The effect of heat recovery on the optimal values of helicopter turboshaft engine parameters
Omar H.H., Kuz'michev V.S., Zagrebelnyi A.O., Grigoriev V.A.
Design procedure of fundamental parameters of the direct-flow detonation pulsing engine
Porshnev V.A.
Multi-purpose high-precision thermal vacuum testing bench and someresults of firing tests of non-hypergolic low-thrust rocket engines
Ryzhkov V.V., Verjasov Y.N., Galperin R.N., Gulyaev Y.I., Ivashin Y.S.
Determination of the optimal parameters and engine layout for a strike unmanned aerial vehicle
Zinenkov Y.V., Lukovnikov A.V., Agaverdyev S.V.
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.
Research of gas turbine engine operation in dust-filled atmosphere
Abdullin B.R., Akmaletdinov R.G., Goumerov K.S., Nigmatullin R.R.
Optimization features of the working process parameters of bypass engine on the basis of given gas generator
Rybakov V.N.
Influence of the initial design data uncertainty on the choice of optimal working process parameters of gas turbine engine
Kuzmichev V.S., Tkachenko A.Y., Rybakov V.N., Krupenich I.N., Kulagin V.V.
Efficiency of using electric propulsion engines for the task of keeping in a near-circular orbit
Ishkov S.A.
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.
Dynamic analysis and optimization of turbojet engine nozzle control mechanism
Spacecraft preset orbital parameters control by means of thrusters
Salmin V.V., Volotsuev V.V., Shikhanov S.V.
Peculiarities of computer modeling of the working process in small gas turbine engines
Kuz'michev V.S., Tkachenko A.Y., Ostapyuk Y.A.
Refining methods of vibration diagnostics of wear of turbo-prop engine differential speed reduction unit gear teeth
Avramenko A.A., Kryuchkov A.N., Plotnikov S.M., Sundukov E.V., Sundukov A.E.
Check and prediction of gas-turbine engine’s technical state
Zotin N.A.
Investigation of energy parameters of small-thrust liquid rocket engines with the geometric expansion ratio of the nozzle F=200
Ageenko Y.I., Nigodyuk V.E., Ryzhkov V.V., Sulinov A.V., Shustov S.A.
Vortex gas wind-driven power plant for supplying compressor stations with electrical energy
Biryuk V.V., Zubrilin I.A., Krasnorutskiy A.S.
Gas turbine engine designing on the basis of a unified gas generator
Rybakov V.N.
Estimate of key parameters of a gas turbine engines with application of the modelling procedure of the equilibrium state of homogeneous mixture of hydrocarbon fuel combustion products
Boldyrev O.I., Gorynov I.M.
1 - 22 of 22 Items

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