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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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
Заболотнов, Ю. М.
Issue
Section
Title
File
Vol 9, No 1 (2010)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Statistical analysis of a capsule’s motion during its reentry into the atmosphere with the aid of a space tether system
(Rus)
Vol 15, No 1 (2016)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Optimal stabilization of small spacecraft angular motion in the process of deployment of an orbital tether system
(Rus)
Vol 15, No 2 (2016)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Analysis of motion stability of a deployed space tether system with an atmospheric probe
(Rus)
Vol 16, No 2 (2017)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Control over the deployment of an orbital tether system of great length
(Rus)
Vol 19, No 1 (2020)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Optimizing the process of changing spacecraft orbital parameters by using a spinning electrodynamic tether sytem
(Rus)
Vol 20, No 2 (2021)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Deployment and stabilization of the motion of a space tethered system in a lunar orbit
(Rus)
Vol 21, No 3 (2022)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Formation of a rotating ring-shaped three-body tethered nanosatellite system with limited control
(Rus)
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