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
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
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Рыжова, И. П.
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Vol 18, No 2 (2019)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Reducing the influence of interference of spacecraft magnetic field on magnetic measurements
(Rus)
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