VESTNIK of Samara University.
Aerospace and Mechanical Engineering
ISSN 2542-0453 (Print)
ISSN 2541-7533 (Online)
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Combustion chamber
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algorithm
blade
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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
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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Vol 9, No 1 (2010)
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Analysis of plane motion relative to the centre of mass of a descent capsule with the three-harmonic moment characteristics during its reentry
>
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Analysis of plane motion relative to the centre of mass of a descent capsule with the three-harmonic moment characteristics during its reentry - PDF (Russian)
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