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
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
optimization
residual stresses
simulation
spacecraft
structure
turbine
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Keywords
Combustion chamber
Gas turbine engine
Mathematical model
Spacecraft
algorithm
blade
combustion chamber
design
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
modeling
optimization
residual stresses
simulation
spacecraft
structure
turbine
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Author Details
Author Details
Проданов, М. Е.
Issue
Section
Title
File
Vol 5, No 2-2 (2006): Special Issue
TECHNICAL SCIENCES
Development of the techical requrement forming and validation technique in the GTE through course computer designing
(Rus)
Vol 5, No 2-2 (2006): Special Issue
TECHNICAL SCIENCES
Development of the technique of gas turbine engines' data storage structure forming
(Rus)
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 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
On the structural and object approaches to modern training for the aerospace industry
(Rus)
Vol 10, No 3-2 (2011): Special Issue
HUMANITIES
Education organization in common information sphere given about product
(Rus)
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