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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deformation
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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
Kirpichev, V. A.
Issue
Section
Title
File
Vol 5, No 2-2 (2006): Special Issue
TECHNICAL SCIENCES
Use of criterion average residual stresses for forecasting a limit of endurance of details at the increased temperature
(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 5-1 (2012): Special Issue
CONFERENCE MATERIALS
Fatigue strength prediction of surface - hardened cylindrical specimens of different diameters
(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 17, No 2 (2018)
MECHANICAL ENGINEERING
Prediction of endurance limit of hardened parts with account of operational factors
(Rus)
Vol 18, No 3 (2019)
MECHANICAL ENGINEERING
Determining the rheological properties of viscoelastic materials by the values of creep strain
(Rus)
Vol 23, No 2 (2024)
MECHANICAL ENGINEERING
Assessment of the endurance limit of light structural metal components using the fatigue surface development method
(Rus)
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