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
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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
Bukaty, A. S.
Issue
Section
Title
File
Vol 5, No 2-2 (2006): Special Issue
TECHNICAL SCIENCES
Prognostication of the technological residual deformations of slim disks after strengthening by means of superficial plastic straining
(Rus)
Vol 12, No 3-2 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Dynamic method of investigating stress concentrators of the YMZ-238 engine crankshaft considering surface hardening plastic deformation
(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 14, No 3-2 (2015): Special Issue
ISSUE WITHOUT SECTION
Calculation methods of investigating the surface layer of thin-walled shafts hardened by methods of surface plastic deformation
(Rus)
Vol 15, No 3 (2016)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Development of the criteria of analyzing the stress-strain state of gas turbine engine parts in the elastoplastic range
(Rus)
Vol 17, No 3 (2018)
MECHANICAL ENGINEERING
Residual stress optimization of technological processes with the aim of ensuring adhesion of nickel or chromium coatings on parts made of titanium alloys
(Rus)
Vol 10, No 3-2 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Experiment-calculated research of the influence of the shot-peening strengthening upon the low-cycle fatigue of the gas turbine parts with the stress concentrator
(Rus)
Vol 10, No 3-2 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
The development of the optimization methodology of the turbine blade-disk interlock of the type “fir tree”
(Rus)
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