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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gas turbine engine
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
Khramov, A. A.
Issue
Section
Title
File
Vol 10, No 2 (2011)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Optimum programs of correction of quasielliptical and circular orbits of spacecraft with the limited-thrust engine
(Rus)
Vol 16, No 3 (2017)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Optimization of space vehicle trans-atmospheric motion by using the method of sequential linearization
(Rus)
Vol 17, No 1 (2018)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Optimizing a vehicle trans-atmospheric motion using Pontryagin’s maximum principle
(Rus)
Vol 17, No 2 (2018)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Optimization of space vehicle combined orbital plane change maneuver on the basis of the successive linearization method
(Rus)
Vol 18, No 1 (2019)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Optimization of space vehicle combined orbital plane change maneuver on the basis of pontryagin’s maximum principle
(Rus)
Vol 18, No 4 (2019)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Application of differential evolution algorithm in the problem of aeroassisted orbital plane change maneuver
(Rus)
Vol 23, No 1 (2024)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Optimization of trajectory motion of the first stage of an aerospace system
(Rus)
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