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
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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
Kulagin, V. V.
Issue
Section
Title
File
Vol 5, No 2-2 (2006): Special Issue
TECHNICAL SCIENCES
Automated system of gas turbine engines termogazdynamic calculation and analysis
(Rus)
Vol 5, No 2-2 (2006): Special Issue
TECHNICAL SCIENCES
Automated variant aircraft GTE turbocompressor flow path designing
(Rus)
Vol 11, No 5-1 (2012): Special Issue
CONFERENCE MATERIALS
Investigation of relative geometric parameters influence on bypass engine mass
(Rus)
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 3-2 (2012): Special Issue
CONFERENCE MATERIALS
The task of creating the bypass engines of various thrust levels using the given gas generator
(Rus)
Vol 11, No 3-3 (2012): Special Issue
CONFERENCE MATERIALS
Improving the efficiency of gas turbines by regenerating heat
(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 3-4 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Preliminary study of principles of effective efficiency change of turboshaft engines of various schemes with heat recovery and intermediate cooling of working medium
(Rus)
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