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
Абульханов, С. Р.
Issue
Section
Title
File
Vol 10, No 3-1 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
A device for diamond smoothing of holes with a centrifugal-force-loaded smoothing tool
(Rus)
Vol 11, No 5-1 (2012): Special Issue
CONFERENCE MATERIALS
Optimization of strength characteristics of lighting devices aircraft by construction of virtual models
(Rus)
Vol 11, No 3-1 (2012): Special Issue
CONFERENCE MATERIALS
Linear mathematical model for the determination of rational treatment conditions on the diamond smoothing operations in the manufacture of aircraft parts
(Rus)
Vol 11, No 3-3 (2012): Special Issue
CONFERENCE MATERIALS
The formation of the contoured surface roughness level of optical purity by using a CNC machine
(Rus)
Vol 13, No 5-4 (2014): Special Issue
ISSUE WITHOUT SECTION
Optimization of the design of a railway searchlight in the ANSYS software environment
(Rus)
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