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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algorithm
blade
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endurance limit
experiment
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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
Igolkin, A. A.
Issue
Section
Title
File
Vol 5, No 2-2 (2006): Special Issue
TECHNICAL SCIENCES
Research of acoustic characteristics of material МR
(Rus)
Vol 13, No 1 (2014)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Modeling static and dynamic characteristics of pressure reducing valves
(Rus)
Vol 11, No 3-1 (2012): Special Issue
CONFERENCE MATERIALS
Pressure pulsation dampener for air controller
(Rus)
Vol 11, No 3-2 (2012): Special Issue
CONFERENCE MATERIALS
The development of mathematical models of acoustic characteristics of the elastic porous material «metal-rubber»
(Rus)
Vol 17, No 2 (2018)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Modal analysis of the dynamic mockup of “AIST–2D” small spacecraft
(Rus)
Vol 1, No 1 (2002)
TECHNICAL SCIENCES
Research of influencing of air delivery in a suction pipe line of the centrifugal pump on its vibroacoustical response
(Rus)
Vol 1, No 1 (2002)
TECHNICAL SCIENCES
Research of influencing of air delivery in a suction pipe line of the centrifugal pump on its vibroacoustical response
(Rus)
Vol 19, No 4 (2020)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Development of improved performance electromagnetic valve for liquid rocket engine
(Rus)
Vol 20, No 2 (2021)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Mathematical model of acoustic characteristics of polyurethane foam used for sound absorption in aerospace engineering
(Rus)
Vol 22, No 3 (2023)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Modal analysis of a spacecraft solar panel
(Rus)
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