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
Gromakovsky, D. G.
Issue
Section
Title
File
Vol 5, No 2-2 (2006): Special Issue
TECHNICAL SCIENCES
Using of the liquids with the high absorbing ability in lamellar vibration isolators
(Rus)
Vol 5, No 2-2 (2006): Special Issue
TECHNICAL SCIENCES
Development of techniques and means of estimating the activation parameters of destruction of surface layers by scratching method
(Rus)
Vol 8, No 3-1 (2009): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Working out the system of technical decisions for ensuring the reliability of friction units of gas-turbine engines
(Rus)
Vol 8, No 4 (2009)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Wave gearing in valve electric drives
(Rus)
Vol 11, No 3-1 (2012): Special Issue
CONFERENCE MATERIALS
Methods of increase of wear resistance and vibroakusticheskikh of parameters of knots of the friction of space equipment
(Rus)
Vol 15, No 3 (2016)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Improvement of adhesive properties and load capacity of the lubricant layer of friction units
(Rus)
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