Author Details

Соловьева, А. В.

Issue Section Title File
Vol 12, No 3-1 (2013): Vestnik SSAU ISSUE WITHOUT SECTION Conditions of compatibility of compressor and turbine used as part of a gas generator required to ensure turbine operability PDF
(Rus)
Vol 6, No 2 (2007): Special Issue TECHNICAL SCIENCES Computational method of the gas flow turbulence intensity at the gas turbine engine combustion chamber outlet PDF
(Rus)
Vol 6, No 2 (2007): Special Issue TECHNICAL SCIENCES Effect of the inlet flow gas temperature field and turbulence on heat transfer in the turbine nozzle cascade and combustion chamber optimization PDF
(Rus)
Vol 10, No 5 (2011) ISSUE WITHOUT SECTION The concept of matching the joint operation of the combustion chamber, the compressor and the turbine PDF
(Rus)
Vol 16, No 2 (2017) AIRCRAFT AND SPACE ROCKET ENGINEERING Formulas of reducing engine environmental performance and combustion characteristics to standard atmospheric conditions PDF
(Rus)
Vol 17, No 4 (2018) AIRCRAFT AND SPACE ROCKET ENGINEERING Theory and calculation of parameters of the detonation engine thermodynamical cycle PDF
(Rus)
Vol 18, No 1 (2019) AIRCRAFT AND SPACE ROCKET ENGINEERING Gas dynamic calculation of detonation in variable cross-section ducts PDF
(Rus)
Vol 18, No 2 (2019) AIRCRAFT AND SPACE ROCKET ENGINEERING Theory of gas turbine engine optimal gas generator PDF
(Rus)
Vol 10, No 3-2 (2011): Special Issue AIRCRAFT AND SPACE ROCKET ENGINEERING Methodology of optimization of parameter of matching the combustion chamber and turbine joint operation PDF
(Rus)
Vol 18, No 3 (2019) AIRCRAFT AND SPACE ROCKET ENGINEERING Gas dynamic calculation of detonation in constant-cross-section ducts PDF
(Rus)

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