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
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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
Паровай, Е. Ф.
Issue
Section
Title
File
Vol 11, No 3-2 (2012): Special Issue
CONFERENCE MATERIALS
Designing of the aviation engine's hydrodynamic bearing
(Rus)
Vol 11, No 3-2 (2012): Special Issue
CONFERENCE MATERIALS
Aviation engine’s hydrodynamic bearing modeling
(Rus)
Vol 13, No 5-1 (2014): Special Issue
ISSUE WITHOUT SECTION
Calculation method for determining the characteristics of elastic-damping suspension made of metal analoque of rubber for plain bearings
(Rus)
Vol 13, No 5-2 (2014): Special Issue
ISSUE WITHOUT SECTION
Designing of low-flow rate slider bearings for turbomachinery rotors
(Rus)
Vol 14, No 3-2 (2015): Special Issue
ISSUE WITHOUT SECTION
Topical issues of gas turbine engine friction unit reliability
(Rus)
Vol 10, No 3-3 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Aircraft engine design based on unified gas generator
(Rus)
Vol 21, No 2 (2022)
MECHANICAL ENGINEERING
Influence of pad geometry and method of oil supply on the thermal state of GTE rotor tilting-pad journal bearing
(Rus)
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