Author Details

Федорченко, Д. Г.

Issue	Section	Title	File
Vol 5, No 2-1 (2006): Special Issue	TECHNICAL SCIENCES	Liquid propellant rocket engines designed by N.D. Kuznetsov Сompany	(Rus)
Vol 5, No 2-2 (2006): Special Issue	TECHNICAL SCIENCES	Structural – technological characteristics of sound-absorbing constructions of the engine NK-93 air inlet duct	(Rus)
Vol 8, No 3-2 (2009): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	Application’s ways of gas–turbine power plants of NK-family for upgrading of heat electric generation plant	(Rus)
Vol 8, No 3-3 (2009): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	Cycle air heating system of gas pumping unit NEVA-25NK	(Rus)
Vol 12, No 3-2 (2013): Vestnik SSAU	ISSUE WITHOUT SECTION	Results of primary operation of NK-37 engine low emission combustion system	(Rus)
Vol 11, No 3-2 (2012): Special Issue	CONFERENCE MATERIALS	The task of creating the bypass engines of various thrust levels using the given gas generator	(Rus)
Vol 13, No 4 (2014)	MECHANICAL ENGINEERING AND POWER ENGINEERING	Heat-shielding zirconium dioxide coating on an intermetallic substrate obtained by the method of high-energy plasma spraying for gas-turbine engine turbine blades	(Rus)
Vol 13, No 5-1 (2014): Special Issue	ISSUE WITHOUT SECTION	Analysis of the thermal state of aircraft engine supports	(Rus)
Vol 13, No 5-3 (2014): Special Issue	ISSUE WITHOUT SECTION	Influence of vibration conectedness on eigenmode shapes of bladed disks with non-identical blades	(Rus)
Vol 13, No 5-4 (2014): Special Issue	ISSUE WITHOUT SECTION	Formation of spread in resonance stresses in bladed disks with non-identical blades and loose vibration conectedness	(Rus)
Vol 13, No 5-4 (2014): Special Issue	ISSUE WITHOUT SECTION	Calculation of exciting aerodynamic load on a gas turbine engine compressor blade induced by the effect of a non-uniform gas flow	(Rus)
Vol 15, No 4 (2016)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Development of an exhaust air turbine engine	(Rus)
Vol 18, No 1 (2019)	MECHANICAL ENGINEERING	Application of additive technology of selective laser melting (SLM) in designing a low emission combustion chamber of a gas turbine plant	(Rus)
Vol 19, No 1 (2020)	MECHANICAL ENGINEERING	New technologies implemented in the design of a low-emission combustion chamber of a gas-turbine unit	(Rus)

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