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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algorithm
blade
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Keywords
Combustion chamber
Gas turbine engine
Mathematical model
Spacecraft
algorithm
blade
combustion chamber
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
optimization
residual stresses
simulation
spacecraft
structure
turbine
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Хазбулатов, А. И.
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Vol 10, No 5 (2011)
ISSUE WITHOUT SECTION
Research of the process of cleaning gas from mechanical impurities in a direct flow centrifugal separator
(Rus)
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