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
Радько, В. М.
Issue
Section
Title
File
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 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 1, No 1 (2002)
TECHNICAL SCIENCES
Gas-dynamic design of brake steps for axial microturbines
(Rus)
Vol 2, No 1 (2003)
TECHNICAL SCIENCES
DETERMINING GEOMETRICAL PARAMETERS OF CENTRIPETAL MICROTURBINE NOZZLE CONSISTING OF RECTILINEAR BLADES
(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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