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
combustion chamber
deformation
design
efficiency
endurance limit
experiment
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gas turbine engine
mathematical model
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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
Чирков, А. В.
Issue
Section
Title
File
Vol 5, No 2-2 (2006): Special Issue
TECHNICAL SCIENCES
Nozzle with a property of shape memory
(Rus)
Vol 8, No 1 (2009)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Increasing the reliability of aircraft components by regulating technological residual stress
(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
Fatigue strength prediction of surface - hardened cylindrical specimens of different diameters
(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 4 (2012)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Modeling dynamic processes of response of fuel pressure-operated valves of superheavy launch vehicles in the tasks of providing structural strength
(Rus)
Vol 10, No 3-3 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Modeling of redistribution of residual stresses in the cylindrical specimens after advancing surface plastic forming
(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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