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
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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
Ravikovich, Yu. A.
Issue
Section
Title
File
Vol 11, No 2 (2012)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Some peculiarities of high-altitude starting of engines of the RD-33 type
(Rus)
Vol 16, No 3 (2017)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Constructing 3D fan blade models in CAD-system on the basis of coordinate measuring techniques
(Rus)
Vol 17, No 4 (2018)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Automated construction of a fan blade model according to data of CAD profile measurements
(Rus)
Vol 18, No 4 (2019)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Verification of a design model and evaluation of a technique of manufacturing aircraft engine composite parts on the basis of dynamic tests
(Rus)
Vol 22, No 3 (2023)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Bench tests of an electric engine-propeller group, as the first stage in the creation of a hybrid power plant
(Rus)
Vol 23, No 2 (2024)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Method of first-approximation calculation of take-off weight of a light aircraft with a hybrid propulsion system
(Rus)
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