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
Темис, Ю. М.
Issue
Section
Title
File
Vol 10, No 3-1 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Numerical investigetion of a non-contacting finger seal
(Rus)
Vol 10, No 3-1 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Rotor in gas bearings dynamics experiment-calculated investigation
(Rus)
Vol 10, No 3-1 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
GTE parts optimal design
(Rus)
Vol 14, No 3-1 (2015): Special Issue
ISSUE WITHOUT SECTION
Application of the invariant plastic flow theory for mathematical modeling of the processes of testing specimens under complex elastic-plastic deformation
(Rus)
Vol 14, No 3-1 (2015): Special Issue
ISSUE WITHOUT SECTION
Dynamic modelling of non-linear vibrations in cylindrical tooth gearing of aircraft drive systems
(Rus)
Vol 14, No 3-1 (2015): Special Issue
ISSUE WITHOUT SECTION
Calculation of the performance of a coulomb friction damper of a crown bevel gear wheel for different forms of resonant oscillations
(Rus)
Vol 10, No 6 (2011)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Numerical simulation of the thermal-stress state of an highpressure compressor rotor with consideration for secondary flows
(Rus)
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