Author Details

Виноградов, А. С.

Issue	Section	Title	File
Vol 8, No 3-1 (2009): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	Seal designing in a structure of the cooling system in gas turbine engine	(Rus)
Vol 8, No 3-1 (2009): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	Research of a seal work as an element of the air engine support	(Rus)
Vol 8, No 3-1 (2009): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	About the thermal protection of the oil cavities for designing gas turbine engines	(Rus)
Vol 10, No 2 (2011)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Research of gasodynamic seal characteristics under transient conditions of aircraft engines and power plants	(Rus)
Vol 10, No 2 (2011)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Designing a seal as an element of air secondary system in aircraft engines	(Rus)
Vol 11, No 3-3 (2012): Special Issue	CONFERENCE MATERIALS	Research of radial face contact seal tightness in the support of the aircraft engine compressor at various operational modes	(Rus)
Vol 11, No 3-3 (2012): Special Issue	CONFERENCE MATERIALS	Seal designing as element of aircraft engine systems and engine units	(Rus)
Vol 13, No 5-1 (2014): Special Issue	ISSUE WITHOUT SECTION	Analysis of the thermal state of aircraft engine supports	(Rus)
Vol 14, No 3-2 (2015): Special Issue	ISSUE WITHOUT SECTION	Research of serviceability of pulsed face seals with pumpback structures	(Rus)
Vol 10, No 3-3 (2011): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	Aircraft engine design based on unified gas generator	(Rus)