Author Details

Данилин, А. И., Самарский государственный аэрокосмический университет имени академика С.П. Королёва (национальный исследовательский университет), Russian Federation

Issue	Section	Title	File
Vol 3, No 1 (2004)	TECHNICAL SCIENCES	Metodical error of the optical-electronic discrete-phase method of turbomachine blades deformation measurement	(Rus)
Vol 7, No 3 (2008): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	The devices for the diagnosis and control of turbine blades deformative condition during operation	(Rus)
Vol 8, No 1 (2009)	MECHANICAL ENGINEERING AND POWER ENGINEERING	Criteria of discrete phase control of blade working condition and their feasibility in systems of turbine driven set automatic control	(Rus)
Vol 9, No 4 (2010)	MECHANICAL ENGINEERING AND POWER ENGINEERING	Energy optimality criteria	(Rus)
Vol 10, No 1 (2011)	ELECTRONICS, MEASURING EQUIPMENT, RADIO ENGINEERING AND COMMUNICATION	Discrete-phase movement transducers for the determination of turbine blade vibration parameters	(Rus)
Vol 10, No 1 (2011)	ELECTRONICS, MEASURING EQUIPMENT, RADIO ENGINEERING AND COMMUNICATION	Technique of operational monitoring of blade operational life exhaustion on turbounits	(Rus)
Vol 13, No 2 (2014)	ISSUE WITHOUT SECTION	Primary converters for the implementation of Doppler method for measuring blade oscillation power unit	(Rus)
Vol 13, No 2 (2014)	ISSUE WITHOUT SECTION	Circuit design receipt autodynes signal to converter displacement parameters elements rotating parts of turbune unit	(Rus)
Vol 13, No 2 (2014)	ISSUE WITHOUT SECTION	Discrete phase converters moving elements rotating units power units	(Rus)
Vol 11, No 3-2 (2012): Special Issue	CONFERENCE MATERIALS	Doppler method for measuring fluctuations of elements rotationg parts power	(Rus)
Vol 11, No 5-2 (2012): Special Issue	CONFERENCE MATERIALS	The device for the determination of blades oscillation parameters based on nonlinear approximation of primary transducers signals	(Rus)
Vol 11, No 7 (2012)	ISSUE WITHOUT SECTION	Parameters transducers of the blade’s dynamic movements of turbounits based on nonlinear approximation of primary signals	(Rus)

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