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
Сурков, О. С.
Issue
Section
Title
File
Vol 8, No 3-3 (2009): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Increase of efficiency of technological preparation of manufacture on the basis of through use of the information technology
(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 13, No 5-3 (2014): Special Issue
ISSUE WITHOUT SECTION
Research of machinability of heat resistant steels 10Х11НN23T3MР-ВД used in parts of gas turbine engines
(Rus)
Vol 10, No 3-3 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
The phenomenological models of the dynamic recrystallization of alloys for aviation
(Rus)
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