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
Сазонов, М. Б.
Issue
Section
Title
File
Vol 5, No 2-1 (2006): Special Issue
TECHNICAL SCIENCES
Optimization of the residai stress in the surface layer of the blades is the method of the increasing reliability and resource
(Rus)
Vol 8, No 3-2 (2009): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
FMS-3000, programming amilling machine 6M13GN-1 a program controller
(Rus)
Vol 11, No 3-1 (2012): Special Issue
CONFERENCE MATERIALS
End mill design and manufacturing with modern multi-axis grinding machines
(Rus)
Vol 11, No 3-1 (2012): Special Issue
CONFERENCE MATERIALS
Research of influence of methods SPD on stpucture surface layer and resistance of fatigue
(Rus)
Vol 11, No 3-3 (2012): Special Issue
CONFERENCE MATERIALS
The formation of the contoured surface roughness level of optical purity by using a CNC machine
(Rus)
Vol 11, No 5-2 (2012): Special Issue
CONFERENCE MATERIALS
Influence of the strengthening-finishing treatment on structure-energy state of surface layer and fatigue resistance
(Rus)
Vol 14, No 3-2 (2015): Special Issue
ISSUE WITHOUT SECTION
Estimation of tension of the surface layer of parts after hardening by different methods of surface plastic deformation
(Rus)
Vol 18, No 1 (2019)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Influence of the stressed state of the surface layer on the endurance of gas turbine engine compressor blades
(Rus)
Vol 10, No 3-3 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Control metods of hardening process in the time of SPD
(Rus)
Vol 20, No 4 (2021)
MECHANICAL ENGINEERING
Research on end mill vibration in machining of VT9 titanium alloy
(Rus)
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