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
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
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simulation
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Keywords
Combustion chamber
Gas turbine engine
Mathematical model
Spacecraft
algorithm
blade
combustion chamber
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
optimization
residual stresses
simulation
spacecraft
structure
turbine
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Author Details
Author Details
Vakulyuk, V. S.
Issue
Section
Title
File
Vol 12, No 1 (2013)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Analysis of the results of fatigue tests of cylindrical specimens with fillets using the method of finite element modeling
(Rus)
Vol 8, No 1 (2009)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Forecasting the endurance limit of shot-strengthened parts with a concentrator by residual stresses of a control specimen
(Rus)
Vol 8, No 1 (2009)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Increasing the reliability of aircraft components by regulating technological residual stress
(Rus)
Vol 13, No 5-1 (2014): Special Issue
ISSUE WITHOUT SECTION
Dependence of the endurance limit on the character of residual stresses distribution in the surface layer of hardened parts
(Rus)
Vol 13, No 5-4 (2014): Special Issue
ISSUE WITHOUT SECTION
Assessing the influence of surface hardening on the endurance limit of specimens made of steel 40X using residual stresses of reference specimen
(Rus)
Vol 17, No 1 (2018)
MECHANICAL ENGINEERING
Residual stresses and fatigue resistance of toothed wheels
(Rus)
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