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
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algorithm
blade
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deformation
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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
Pavlova, S. A.
Issue
Section
Title
File
Vol 19, No 3 (2020)
MECHANICAL ENGINEERING
Optimization of honeycomb sandwich floor panels made of polymer-matrix low-combustible composite materials based on high-strength carbon and glass fibers and adhesive binder
(Rus)
Vol 20, No 1 (2021)
MECHANICAL ENGINEERING
Analysis of contact interaction of polymer honeycomb core and CFRP base layers in sandwich-core constructions
(Rus)
Vol 20, No 2 (2021)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Optimal design of sandwich floor panels made of high-strength composite materials considering stiffness constraints
(Rus)
Vol 21, No 2 (2022)
MECHANICAL ENGINEERING
Experimental and analytical determination of the elastic characteristics of layered woven composites
(Rus)
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