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The concept of matching the joint operation of the combustion chamber, the compressor and the turbine
Grigoriev A.V., Golubchikov P.P., YIlushin M.Y., Rudakov O.A., Solovieva A.V.
The efficiency of aligning gratings at engine inlet of ground power plants
,
Calculation of exciting aerodynamic load on a gas turbine engine compressor blade induced by the effect of a non-uniform gas flow
Ermakov A.I., Shklovets A.O., Fedorchenko D.G.
Mathematical model for calculating radial non-uniformity of the gas temperature field at the exit of small gas turbine engine combustion chambers
Lukachev S.V., Abrashkin V.Y., Lansky A.M., Matveev S.G.
Reduction of variable resonance stresses in the last stage of medium pressure compressor
Shklovets A.O., Sen'chev M.N., Dzhibilov P.T.
Correlation and regression model for the assessment of circular non-uniformity of the gas temperature field at the outlet of small gas turbine engine combustion chambers
Lukachev S.V., Abrashkin V.Y., Lansky A.M., Matveev S.G.
Reduction of circumferential variation in the final stage of IPC
Baturin O.V., Krivcov A.V., Matveev V.N., Popov G.M.
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.
Choice of gas temperature at the turbopump turbine inlet
Ivanov A.V.
Experimental study of air flow in axisymmetric diffuser output section with rotating wall
Kurkin E.I., Ivchenko A.V.
Methodology of optimization of parameter of matching the combustion chamber and turbine joint operation
Grigoriev A.V., Golubchikov P.P., Ilushin M.Y., Rudakov O.A., Solovieva A.V.
Experimental investigation of turbulence of influence of the compressor’s out flow parameters on the hydraulics parameters resistance of separation diffuser of combustion chamber
Guryanova M.M.
Generation of signals with prescribed spectral characteristics
Baraboshin A.Y., Minaeva O.A.
Peculiarities of gas temperature field formation at the exit of small-sized gas turbine engine combustion chambers
1 1., 1 1., 1 1.
1 - 14 of 14 Items

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