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
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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
Ларионова, Ю. С.
Issue
Section
Title
File
Vol 11, No 5-1 (2012): Special Issue
CONFERENCE MATERIALS
Research of notch radius and depth influence on residual stresses distribution character in the smallest cross-section of surface hardened detail
(Rus)
Vol 11, No 3-3 (2012): Special Issue
CONFERENCE MATERIALS
Residual stresses distribution regularities in the smallest section of hardened hollow cylindrical detail with circular cut
(Rus)
Vol 10, No 3-3 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Modeling of redistribution of residual stresses in the cylindrical specimens after advancing surface plastic forming
(Rus)
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