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
Zhidyaev, A. N.
Issue
Section
Title
File
Vol 10, No 2 (2011)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Research of errors of measuring angular location parameters of holes in turbine and compressor discs of gas turbine engines
(Rus)
Vol 11, No 3-2 (2012): Special Issue
CONFERENCE MATERIALS
Technological processes simulation incomplex parts production of aerospacetechnical equipment: problems and the ways of their solving
(Rus)
Vol 11, No 3-2 (2012): Special Issue
CONFERENCE MATERIALS
NC machine tools contact measuring devices uncertainty when products geometrical parameters control
(Rus)
Vol 11, No 5-2 (2012): Special Issue
CONFERENCE MATERIALS
Milling and microballs strengthening conditions influence on high-temperature alloies and steels part’s coating surface quality experimental investigation
(Rus)
Vol 10, No 3-3 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Measurment procedure optimizing geometrical parameters of measure GTE feature on coordinate measuring machine
(Rus)
Vol 20, No 4 (2021)
MECHANICAL ENGINEERING
Research on end mill vibration in machining of VT9 titanium alloy
(Rus)
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