Author Details

Baturin, O. V.

Issue	Section	Title	File
Vol 7, No 3 (2008): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	Calculated study of tangential inclination of nozzle vanes influence on gas-dynamic efficiency of axial turbine stage	(Rus)
Vol 8, No 3-1 (2009): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	Formation of a structural calculated mesh the passage blade of the axial turbine in program GAMBIT	(Rus)
Vol 11, No 5-1 (2012): Special Issue	CONFERENCE MATERIALS	Simulation of aircraft multistage axial turbine working processes taking into account over-shroud leakage flows and blading inflows	(Rus)
Vol 11, No 5-1 (2012): Special Issue	CONFERENCE MATERIALS	Reduction of circumferential variation in the final stage of IPC	(Rus)
Vol 11, No 5-1 (2012): Special Issue	CONFERENCE MATERIALS	Approaches to modeling work of gas turbine engine`s core as a connected task	(Rus)
Vol 11, No 5-1 (2012): Special Issue	CONFERENCE MATERIALS	Optimization of aircraft seven stage compressor first stages parameters	(Rus)
Vol 11, No 3-2 (2012): Special Issue	CONFERENCE MATERIALS	Computational research of multistage turbine flow taking into account flow spatial structure and associated volumes	(Rus)
Vol 11, No 3-2 (2012): Special Issue	CONFERENCE MATERIALS	Selection of optimal configuration and workflow parameters of autonomous micro gas turbine plant	(Rus)
Vol 14, No 3-2 (2015): Special Issue	ISSUE WITHOUT SECTION	Optimization of the workflow of multistage axial turbines with platforms	(Rus)
Vol 14, No 3-2 (2015): Special Issue	ISSUE WITHOUT SECTION	The use of mathematical optimization means to increase the efficiency of a seven-stage axial flow compressor	(Rus)
Vol 10, No 3-3 (2011): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	Determination of a rational combination of the radial turbine basic parameters with an allowance for strength, technological and other constraints	(Rus)
Vol 10, No 3-3 (2011): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	Blading of radial-axial turbine wheel using Bezier curve	(Rus)
Vol 19, No 3 (2020)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Method of coordinating joint operation of air starter and auxiliary power unit and determining the gas turbine engine starting time	(Rus)
Vol 22, No 3 (2023)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Features of design calculation of compressor spool flow path of a twin-shaft gas turbine engine core on the basis of 1D and 2D models of their working process	(Rus)

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