Author Details

Rudakov, О. A.

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	(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	(Rus)
Vol 16, No 2 (2017)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Formulas of reducing engine environmental performance and combustion characteristics to standard atmospheric conditions	(Rus)
Vol 17, No 4 (2018)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Theory and calculation of parameters of the detonation engine thermodynamical cycle	(Rus)
Vol 18, No 1 (2019)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Gas dynamic calculation of detonation in variable cross-section ducts	(Rus)
Vol 18, No 2 (2019)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Theory of gas turbine engine optimal gas generator	(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	(Rus)
Vol 18, No 3 (2019)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Gas dynamic calculation of detonation in constant-cross-section ducts	(Rus)