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
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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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
Grigoryev, V. A.
Issue
Section
Title
File
Vol 5, No 2-2 (2006): Special Issue
TECHNICAL SCIENCES
The automated informative complex for test operation of aviation gas turbine engine
(Rus)
Vol 13, No 5-1 (2014): Special Issue
ISSUE WITHOUT SECTION
Assessing reduction gear mass in the problem of optimizing parameters of the working process of a turboprop engine at the initial design stage
(Rus)
Vol 13, No 5-2 (2014): Special Issue
ISSUE WITHOUT SECTION
Problems of ultralow power turbine design in a turbine drive system
(Rus)
Vol 13, No 5-2 (2014): Special Issue
ISSUE WITHOUT SECTION
Formation of a method of choosing rational values of ultralow power turbine parameters in a turbine drive system
(Rus)
Vol 10, No 6 (2011)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Planning a factorial experiment for testing a single-stage ultralow power turbine
(Rus)
Vol 15, No 4 (2016)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Mathematical models for evaluating the energy efficiency of ultralow power turbine drives
(Rus)
Vol 10, No 6 (2011)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Choise of the range and levels of varying the factors of the experiment plan for testing single-stage ultralow power turbine
(Rus)
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