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
deformation
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
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residual stresses
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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
Zrelov, V. A.
Issue
Section
Title
File
Vol 5, No 2-2 (2006): Special Issue
TECHNICAL SCIENCES
Forming of bearings’ data structure in GTE information sphear
(Rus)
Vol 6, No 1 (2007)
CYBERNETICS AND INFORMATION SCIENCE
Information support of operation stage in the life cycle of aircraft construction items
(Rus)
Vol 8, No 3-1 (2009): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Project of 30 000 h.p. power gas turbine
(Rus)
Vol 11, No 3-2 (2012): Special Issue
CONFERENCE MATERIALS
Working conditions analysis of rotor supports bearings in aviation gas turbine engines and energetic units structure
(Rus)
Vol 11, No 3-3 (2012): Special Issue
CONFERENCE MATERIALS
Experimental research of shaft sealing with elastic element made of MR material
(Rus)
Vol 13, No 5-1 (2014): Special Issue
ISSUE WITHOUT SECTION
Research of shaft seals made of porous wire «metal rubber» material
(Rus)
Vol 23, No 1 (2024)
MECHANICAL ENGINEERING
Development of a mathematical model of the internal structure of a granular heat accumulator for launching a mono-fuel gas generator
(Rus)
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