Author Details

Бердник, О. Б.

Issue	Section	Title	File
Vol 5, No 2-1 (2006): Special Issue	TECHNICAL SCIENCES	Analytical estimation of postoperational condition of high pressure turbine blades of ДЦ 59Л and ДЖ59 engines and their damage control features	(Rus)
Vol 8, No 3-3 (2009): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	Structure and mehanpichesky properties of the shovel 1 steps of the rotor of turbine GTE-45-3 after the long operating time and regeneration	(Rus)
Vol 14, No 3 (2014)	MECHANICAL ENGINEERING AND POWER ENGINEERING	Research of a heat-resistant intermetallic underlayer for the heat-shielding coating of gas turbine engine turbine blades	(Rus)
Vol 13, No 4 (2014)	MECHANICAL ENGINEERING AND POWER ENGINEERING	Post-operation state and extension of service life of compressor blades of the gas-turbine power plant GTE-45-3	(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 10, No 3-2 (2011): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	Structure and physico-mechanical properties of heat resistant gazoplazmennyh coating NiCrCoAlY/ZrO2 for turbine blades of gas turbine engines	(Rus)
Vol 10, No 3-2 (2011): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	Development of technology extension resource ХН65ВМТЮ alloy turbine blades	(Rus)