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
Rybakov, V. N.
Issue
Section
Title
File
Vol 11, No 5-1 (2012): Special Issue
CONFERENCE MATERIALS
Methods and means of aircraft gas turbine engine conceptual design underlying the CAE system «ASTRA»
(Rus)
Vol 11, No 5-1 (2012): Special Issue
CONFERENCE MATERIALS
Problem formulation of bypass engine parameters optimization with a preselected gas generator
(Rus)
Vol 11, No 5-1 (2012): Special Issue
CONFERENCE MATERIALS
Influence of the initial design data uncertainty on the choice of optimal working process parameters of gas turbine engine
(Rus)
Vol 11, No 5-1 (2012): Special Issue
CONFERENCE MATERIALS
Dependence of required turbine inlet temperature at cruise mode of long-term flight on bypass ratio
(Rus)
Vol 11, No 3-3 (2012): Special Issue
CONFERENCE MATERIALS
Optimization features of the working process parameters of bypass engine on the basis of given gas generator
(Rus)
Vol 11, No 3-3 (2012): Special Issue
CONFERENCE MATERIALS
Gas turbine engine designing on the basis of a unified gas generator
(Rus)
Vol 13, No 5-3 (2014): Special Issue
ISSUE WITHOUT SECTION
Computer-aided system of virtual gas turbine engine testing
(Rus)
Vol 10, No 3-3 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Dataware of virtual lab for gas turbine engine testing
(Rus)
Vol 10, No 3-3 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Concept of construction of virtual lab for gas turbine engine testing
(Rus)
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