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
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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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
Vakuljuk, V. S.
Issue
Section
Title
File
Vol 12, No 3-2 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Analysis of stress distribution in the dangerous section area of specimens with fillets under bending using the finite-element modeling method
(Rus)
Vol 11, No 5-1 (2012): Special Issue
CONFERENCE MATERIALS
Nitriding influence on residual stresses and endurance limit of specimens with notches made of 38Х2МЮА steel
(Rus)
Vol 11, No 5-1 (2012): Special Issue
CONFERENCE MATERIALS
Evaluation of thermochemical treatment influence on fatigue strength of specimens under normal and high temperatures
(Rus)
Vol 11, No 3-3 (2012): Special Issue
CONFERENCE MATERIALS
The dependence of detail fatigue resistance on the thickness of hardening layer under outstripping superficial plastic deforming
(Rus)
Vol 10, No 3-3 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Residual stresses in the specimens with opennings imitating openings for coupling bolt into the turbine of jet engines
(Rus)
Vol 10, No 3-4 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Influence of notch radius at advancing surface plastic deforming on endurance limit of detail
(Rus)
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