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
Силуянова, М. В.
Issue
Section
Title
File
Vol 17, No 2 (2018)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Assuring performance characteristics of gas-turbine engine parts and assemblies using electrospark doping
(Rus)
Vol 17, No 2 (2018)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Improvement of friction units of power plants by aplying ceramic composite spray coatings
(Rus)
Vol 18, No 2 (2019)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Calculation of lubricant flow in the slide bearing of the aviation engine reducer
(Rus)
Vol 18, No 3 (2019)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Determining a rational scheme of machining of gas turbine engine essential parts in magnetorheological environments by the method of expert assessment
(Rus)
Vol 19, No 1 (2020)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Method for optimizing mass and size characteristics of a high-pressure turbine disk
(Rus)
Vol 20, No 3 (2021)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Analysis of basic concepts of advanced engines for supersonic civil aircraft on the basis of foreign designers’ experience
(Rus)
Vol 22, No 1 (2023)
AIRCRAFT AND SPACE ROCKET ENGINEERING
The problems of creating a propulsion system of a new generation supersonic passenger aircraft (review)
(Rus)
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