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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Spacecraft
algorithm
blade
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efficiency
endurance limit
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finite element method
gas turbine engine
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Combustion chamber
Gas turbine engine
Mathematical model
Spacecraft
algorithm
blade
combustion chamber
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
mathematical modeling
modeling
optimization
residual stresses
simulation
spacecraft
structure
turbine
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Author Details
Author Details
Павлов, В. Ф., Самарский государственный аэрокосмический университет имени академика С.П. Королёва (национальный исследовательский университет), Russian Federation
Issue
Section
Title
File
Vol 5, No 3 (2006)
TECHNICAL SCIENCES
The influence of the concentrator type on the dependence of endurance limit of strengthened parts on residual stresses
(Rus)
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 11, No 5-1 (2012): Special Issue
CONFERENCE MATERIALS
Fatigue strength prediction of surface - hardened cylindrical specimens of different diameters
(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
Ultrasonic hardening of specimens made of ЭИ698 alloy optimal regimes choice using average integral residual stresses criterion
(Rus)
Vol 11, No 5-2 (2012): Special Issue
CONFERENCE MATERIALS
Speckle interferometry digital research for stress-strain state of objects
(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 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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