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
combustion chamber
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
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Search Scope
All
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Abstract
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Full Text
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By Issue
By Author
By Title
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Other Journals
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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Vol 15, No 4 (2016)
>
Unstady heat-mass-transfer and fuel distributions in flows downstream the gas-dynamic flame holder
>
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Unstady heat-mass-transfer and fuel distributions in flows downstream the gas-dynamic flame holder - PDF (Russian)
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