VESTNIK of Samara University.
Aerospace and Mechanical Engineering
ISSN 2542-0453 (Print)
ISSN 2541-7533 (Online)
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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
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Budnik, S. A.
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Vol 18, No 4 (2019)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Experimental testing of heat flux sensors based on the inverse problem technique
(Rus)
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