Author Details

Букатый, С. А., Рыбинская государственная авиационная технологическая академия имени П.А. Соловьева, Russian Federation

Issue	Section	Title	File
Vol 5, No 2-2 (2006): Special Issue	TECHNICAL SCIENCES	Prognostication of the technological residual deformations of slim disks after strengthening by means of superficial plastic straining	(Rus)
Vol 5, No 2-2 (2006): Special Issue	TECHNICAL SCIENCES	On selection of equivalent loading of standard smooth specimens for determining low-cycle durability of gas-turbine engine major components	(Rus)
Vol 5, No 2-2 (2006): Special Issue	TECHNICAL SCIENCES	Automatical system for determination the residual tensions in the segments of complex forms	(Rus)
Vol 8, No 3-2 (2009): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	The optimization of the turbine blade-disk interlock of the type “fir tree”	(Rus)
Vol 8, No 3-2 (2009): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	the research of the influence of the maximal stress duration in the cycle of loading upon the low-cycle fatigue and the long-term strength of the turbine shaft made of the material ЭИ 961-Ш	(Rus)
Vol 8, No 3-2 (2009): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	The determination of the efficient parameters of surface strenghtening the thin-walled and the small-hard parts of gas turbine engines based on deformation tolerance	(Rus)
Vol 11, No 3-1 (2012): Special Issue	CONFERENCE MATERIALS	The defectoscopy of the fatigue cracks in the gas turbine parts by means of eddy-current method	(Rus)
Vol 13, No 5-4 (2014): Special Issue	ISSUE WITHOUT SECTION	Study of cycle life of a material in conditions of low-cycle fatigue and long-term strength	(Rus)
Vol 13, No 5-4 (2014): Special Issue	ISSUE WITHOUT SECTION	Research of the validity of forecasting low cycle durability of gas turbine engine parts based on Manson’s equation	(Rus)
Vol 10, No 3-2 (2011): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	Experiment-calculated research of the influence of the shot-peening strengthening upon the low-cycle fatigue of the gas turbine parts with the stress concentrator	(Rus)

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