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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blade
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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
Author Details
Popov, P. A.
Issue
Section
Title
File
Vol 12, No 1 (2013)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Peculiarities of acoustic loading of the space vehicle in the nose fairing launched as part of a «Soyuz»-type rocket
(Rus)
Vol 13, No 1 (2014)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Constructive actions for decreasing the acoustic pressure inside space-rocket products
(Rus)
Vol 14, No 3 (2014)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Calculating sound insulation of a sandwich structure on the basis of the «inverse matrix» method
(Rus)
Vol 11, No 4 (2012)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Assessment of changes in the sound-proof ability of the rocket fairing with layers of sound-proof materials varying in thickness
(Rus)
Vol 11, No 4 (2012)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Mathematical model of investigating normal acoustic modes of launch vehicle modules
(Rus)
Vol 16, No 2 (2017)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Application of Bubnov-Galerkin method to determine fixed vibrational loads of launch vehicle compartments
(Rus)
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