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
combustion chamber
deformation
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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
Баринова, Е. В.
Issue
Section
Title
File
Vol 9, No 1 (2010)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Analysis of plane motion relative to the centre of mass of a descent capsule with the three-harmonic moment characteristics during its reentry
(Rus)
Vol 9, No 4 (2010)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Research of spatial motion of an uncontrolled spacecraft with the triharmonic moment characteristics around its center of mass during its reentry into atmosphere
(Rus)
Vol 9, No 4 (2010)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Deviation of reentry spacecraft from the estimated trajectory caused by transient modes of angular motion at the stage of entry into the atmosphere
(Rus)
Vol 18, No 2 (2019)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Relative equilibria of dynamically symmetric CubeSat nanosatellite under the action of aerodynamic and gravitational torques
(Rus)
Vol 21, No 3 (2022)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Procedure of assessing the error of the device for measuring mass-centering and inertial characteristics of nanosatellites using reference objects
(Rus)
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