VESTNIK of Samara University.
Aerospace and Mechanical Engineering
ISSN 2542-0453 (Print)
ISSN 2541-7533 (Online)
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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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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
Вдовин, Р. А.
Issue
Section
Title
File
Vol 11, No 3-3 (2012): Special Issue
CONFERENCE MATERIALS
3d virtual simulation and casting process optimization of part GTE "Swirler of II duct" with using computer technologies
(Rus)
Vol 13, No 5-3 (2014): Special Issue
ISSUE WITHOUT SECTION
Development of a technique of molding small complex parts of gas turbine engines from high-temperature alloys using additive technologies
(Rus)
Vol 14, No 3-2 (2015): Special Issue
ISSUE WITHOUT SECTION
Application of numerical simulation systems for the research of the blade casting process in blank production
(Rus)
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