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
Жильников, Е. П.
Issue
Section
Title
File
Vol 12, No 2 (2013)
MECHANICAL ENGINEERING AND POWER ENGINEERING
The influence of design and performance parameters of an angular ball bearing on the stiffness of gas turbine engine rotor supports
(Rus)
Vol 8, No 3-1 (2009): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Calculation of the double-row spherical roller bearing of the satellite gear wheel of the planetary reducer
(Rus)
Vol 10, No 1 (2011)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Serviceability of the rolling contact of rings and bending strength of textolite cage rivets of ball bearings in helicopter transmission
(Rus)
Vol 11, No 1 (2012)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Calculation of skidding in intershaft roller bearings of gas turbine engines
(Rus)
Vol 10, No 3-3 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Calculation of aircraft high-speed rolling-element bearing rings fit
(Rus)
Vol 10, No 6 (2011)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Calculation of vibroacoustic characteristics of a four-point ball bearing. Part 1
(Rus)
Vol 10, No 6 (2011)
MECHANICAL ENGINEERING
Calculation of vibroacoustic characteristics of a four-point ball bearing. Part 2
(Rus)
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