VESTNIK of Samara University.
Aerospace and Mechanical Engineering
ISSN 2542-0453 (Print)
ISSN 2541-7533 (Online)
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Combustion chamber
Gas turbine engine
Mathematical model
Spacecraft
algorithm
blade
combustion chamber
design
efficiency
experiment
finite element method
gas turbine engine
mathematical model
mathematical modeling
modeling
optimization
residual stresses
simulation
spacecraft
structure
turbine
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Keywords
Combustion chamber
Gas turbine engine
Mathematical model
Spacecraft
algorithm
blade
combustion chamber
design
efficiency
experiment
finite element method
gas turbine engine
mathematical model
mathematical modeling
modeling
optimization
residual stresses
simulation
spacecraft
structure
turbine
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Author Details
Author Details
Тарасенко, Ю. П., ЗАО НПЦ «Трибоника», Нф ИМАШ РАН, г. Нижний Новгород, Russian Federation
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 5, No 2-1 (2006): Special Issue
TECHNICAL SCIENCES
Postoperational condition analysis and overhal-period renewal technology of blades in gas turbine engines and gas-compressor units
(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 11, No 3-1 (2012): Special Issue
CONFERENCE MATERIALS
Nondestructive testing of the working compressor blades of the aviation engine
(Rus)
Vol 11, No 3-1 (2012): Special Issue
CONFERENCE MATERIALS
Technological features of formation of the multifunctional nanostructured coverings of nitride of the titan for compressor shovels aviation GTD
(Rus)
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