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
finite element method
gas turbine engine
mathematical model
modeling
optimization
residual stresses
simulation
structure
turbine
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Abstract
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Search Scope
All
Authors
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Abstract
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Full Text
Browse
By Issue
By Author
By Title
By Sections
Other Journals
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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Vol 14, No 3-1 (2015)
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Application of the cyclic life additivity concept for the determination of service life of aero engine disks made from powder alloys
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Application of the cyclic life additivity concept for the determination of service life of aero engine disks made from powder alloys - PDF (Russian)
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