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
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deformation
design
efficiency
endurance limit
experiment
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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
Author Details
Shabalkin, D. Yu.
Issue
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Vol 11, No 5-1 (2012): Special Issue
CONFERENCE MATERIALS
Basic approaches and requirements to the formation of polyplatform integrated automated system of aircraft life cycle support based on the product electronic definition
(Rus)
Vol 11, No 5-1 (2012): Special Issue
CONFERENCE MATERIALS
Organization of go-ahead engineers training for aircraft industry at the example of the strategic alliance of Ulyanovsk state university and CJSS “Aviastar-SP”
(Rus)
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