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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algorithm
blade
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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
Семёнова, О. Ю.
Issue
Section
Title
File
Vol 7, No 1 (2008)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Impact of smooth part residual stress distribution on additional stresses in case of leading surface plastic deformation
(Rus)
Vol 10, No 1 (2011)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Residual stresses and fatigue resistance of surface-hardened notched cylindrical specimens made of steel 20
(Rus)
Vol 11, No 5-1 (2012): Special Issue
CONFERENCE MATERIALS
Residual stresses and endurance strength in the specimens with V-shaped notches made of ВНС40 steel
(Rus)
Vol 11, No 3-3 (2012): Special Issue
CONFERENCE MATERIALS
Coefficient of residual stresses influence on cylindrical parts endurance limit under bending estimation
(Rus)
Vol 11, No 3-3 (2012): Special Issue
CONFERENCE MATERIALS
Superficial hardened part critical depth of non-propagating fatigue crack evaluation
(Rus)
Vol 13, No 5-3 (2014): Special Issue
ISSUE WITHOUT SECTION
Forecasting an increment in the parts’ endurance limit due to surface hardening
(Rus)
Vol 17, No 2 (2018)
MECHANICAL ENGINEERING
Evaluating the efficiency of hardening treatment of cylindrical parts made of structural steels
(Rus)
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