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
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Spacecraft
algorithm
blade
combustion chamber
deformation
design
efficiency
endurance limit
experiment
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gas turbine engine
mathematical model
modeling
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residual stresses
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Keywords
Combustion chamber
Gas turbine engine
Mathematical model
Spacecraft
algorithm
blade
combustion chamber
deformation
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
optimization
residual stresses
simulation
structure
turbine
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Author Details
Author Details
Tsareva, I. N.
Issue
Section
Title
File
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 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)
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
Research of the postoperational condition of the restored compressor shovels of GTD gas-transfer of the units which have fulfilled the appointed resource
(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
Optimization of the technology of ion-plasma coating of titanium nitride in the small-sized thin-walled details
(Rus)
Vol 10, No 3-2 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Development of technology extension resource ХН65ВМТЮ alloy turbine blades
(Rus)
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