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
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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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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Author Details
Author Details
Хамидуллин, А. Ш.
Issue
Section
Title
File
Vol 14, No 3-1 (2015): Special Issue
ISSUE WITHOUT SECTION
Experimental determination of thermal-fatigue life of turbine blades with various coatings made of an advanced heat resistant nickel alloy
(Rus)
Vol 10, No 3-2 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Estimation of a tension of a columnar thermal barrier coatings on nozzle turbine blades and segments of flame pipes of combustion chambers subject to frictional force between a ceramic layer and gas-dynamic flow
(Rus)
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