VESTNIK of Samara University.
Aerospace and Mechanical Engineering
ISSN 2542-0453 (Print)
ISSN 2541-7533 (Online)
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Combustion chamber
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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
Новиков, Д. К.
Issue
Section
Title
File
Vol 5, No 2-1 (2006): Special Issue
TECHNICAL SCIENCES
Results of experimental tests of «dry» seals for NK-37 gas turвine separate compressor with the use of air as working body
(Rus)
Vol 8, No 3-2 (2009): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Optimization characteristics of rotor-support system from NK-14ST free power turbine with consider statics and dynamics propertys
(Rus)
Vol 14, No 3-2 (2015): Special Issue
ISSUE WITHOUT SECTION
Calculation of the damping coefficient of flexible rings with working fluid
(Rus)
Vol 16, No 1 (2017)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Influence of assembly conditions on the stressed-stained state of damper support elastic rings
(Rus)
Vol 10, No 3-3 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Dynamik experimental researches of the face gas dynamic seal
(Rus)
Vol 20, No 4 (2021)
MECHANICAL ENGINEERING
Determining static stiffness of damper elastic rings
(Rus)
Vol 21, No 3 (2022)
MECHANICAL ENGINEERING
Analysis of the influence of lubricant supply conditions on the pressure distribution in squeeze-film dampers
(Rus)
Vol 23, No 3 (2024)
MECHANICAL ENGINEERING
Experimental determination of damping coefficient of a support with elastic ring under harmonic loading
(Rus)
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