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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algorithm
blade
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deformation
design
efficiency
endurance limit
experiment
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mathematical model
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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
Krikunov, M. M.
Issue
Section
Title
File
Vol 11, No 5-2 (2012): Special Issue
CONFERENCE MATERIALS
Synthesis of dynamic modes of attitude motion of spacecraft with solid propellant rocket engine
(Rus)
Vol 15, No 3 (2016)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Efficiency of terminal control in the trans-atmospheric first stage of an aerospace system under atmospheric and aerodynamic disturbances
(Rus)
Vol 17, No 4 (2018)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Analysis of control programs and flight paths of a hypersonic vehicle in climb
(Rus)
Vol 18, No 1 (2019)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Analysis of control programs and climb paths of the hypersonic first stage of an aerospace system
(Rus)
Vol 18, No 2 (2019)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Disturbed motion of a hypersonic vehicle in climb
(Rus)
Vol 18, No 3 (2019)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Disturbed motion of the hypersonic first stage of an aerospace system in climb
(Rus)
Vol 19, No 1 (2020)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Optimal command control of hypersonic aircraft flight path in conditions of atmospheric disturbances
(Rus)
Vol 19, No 2 (2020)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Optimal command control of flight paths of aerospace system hypersonic first stage in conditions of atmospheric disturbances
(Rus)
Vol 19, No 3 (2020)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Disturbed transatmospheric motion of the first stage of an aerospace system
(Rus)
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