VESTNIK of Samara University.
Aerospace and Mechanical Engineering
ISSN 2542-0453 (Print)
ISSN 2541-7533 (Online)
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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
Кучеров, А. С.
Issue
Section
Title
File
Vol 3, No 2 (2004)
TECHNICAL SCIENCES
Evaluation of changes of gas parameters in a vessel when its wall is broken through by high-velocity mechanicak particles
(Rus)
Vol 9, No 2 (2010): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Task-oriented systems in the problems of spacecrafts designing
(Rus)
Vol 11, No 4 (2012)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Method of choosing spacecraft design characteristics on the basis of creating task-oriented systems of computer-aided design
(Rus)
Vol 13, No 5-3 (2014): Special Issue
ISSUE WITHOUT SECTION
Estimation of mass-dimensional characteristics of a complex propulsion unit of earth remote sensing spacecraft
(Rus)
Vol 15, No 2 (2016)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Metodological basis of the development of a problem-oriented system for selecting design parameters of space vehicles
(Rus)
Vol 15, No 2 (2016)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Procedure of comparative assessment of the efficiency of Earth remote sensing satellites with different optoelectronic telescopic complexes
(Rus)
Vol 22, No 2 (2023)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Simulating the process of retargeting of optoelectronic Earth observation spacecraft during object shooting
(Rus)
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