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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Spacecraft
algorithm
blade
combustion chamber
design
efficiency
endurance limit
experiment
finite element method
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mathematical model
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Keywords
Combustion chamber
Gas turbine engine
Mathematical model
Spacecraft
algorithm
blade
combustion chamber
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
optimization
residual stresses
simulation
spacecraft
structure
turbine
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Author Details
Author Details
Grigoriev, V. A.
Issue
Section
Title
File
Vol 12, No 3-2 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Optimal distribution of turboprop engine free energy between the screw and the jet with mass characteristics taken into account
(Rus)
Vol 11, No 3-3 (2012): Special Issue
CONFERENCE MATERIALS
Application of the artifical neyral networks theory methods for generalization and representation charachteristics of aviation gas turbine engines axial compressors
(Rus)
Vol 11, No 3-3 (2012): Special Issue
CONFERENCE MATERIALS
Volume and mass mathematical models of single-stage centripetal ultralow power turbines
(Rus)
Vol 1, No 1 (2002)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Stability of optimal solutions in the formation of the operation process of small gas-turbine engines for a multipurpose helicopter
(Rus)
Vol 10, No 3-2 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Bases of methodology of maintenance of system safe operation of engines at all stages of life cycle
(Rus)
Vol 19, No 4 (2020)
AIRCRAFT AND SPACE ROCKET ENGINEERING
The effect of heat recovery on the optimal values of helicopter turboshaft engine parameters
(Rus)
Vol 20, No 3 (2021)
JUBILEES OF SCIENTISTS
Artificial intelligence in aircraft design and the role of professor V.G. Maslov’s scientific school in the process of its development
(Rus)
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