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
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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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
Dokukina, I. A.
Issue
Section
Title
File
Vol 8, No 3-1 (2009): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Wearability, wearproof and heat-shielding coverings for details of the gas path of the turbine, the compressor and the chamber of combustion of gas turbine engine
(Rus)
Vol 11, No 5-1 (2012): Special Issue
CONFERENCE MATERIALS
Increase of operational characteristics of details at the expense of depositions plasma thermal spray coatings cluster structure
(Rus)
Vol 11, No 3-1 (2012): Special Issue
CONFERENCE MATERIALS
Management of properties of heat-shielding plasma coverings of details of gas-turbine engines
(Rus)
Vol 11, No 3-1 (2012): Special Issue
CONFERENCE MATERIALS
Selection of the design and application of plasma technology protective coatings parts gas turbine engines
(Rus)
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