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
Печенин, В. А.
Issue
Section
Title
File
Vol 13, No 5-3 (2014): Special Issue
ISSUE WITHOUT SECTION
Improving the accuracy of assessing the position deviation in coordinate measurements of GTE compressor and turbine blade profiles
(Rus)
Vol 14, No 3-2 (2015): Special Issue
ISSUE WITHOUT SECTION
Comparative research of algorithms of measuring the geometry of complex profiles of gas turbine engine compressor blades
(Rus)
Vol 15, No 2 (2016)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Study of uncertainty of measuring geometrical parameters of gas turbine engine compressor blade profiles
(Rus)
Vol 15, No 4 (2016)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Technique of compensating errors in machining of parts with sculptured surfaces
(Rus)
Vol 18, No 2 (2019)
MECHANICAL ENGINEERING
Prediction of product assembly errors using real part models
(Rus)
Vol 19, No 1 (2020)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Algorithm for predicting the vibrational state of a turbine rotor using machine learning
(Rus)
Vol 22, No 2 (2023)
MECHANICAL ENGINEERING
Development of a model for determination of preloads on blade shrouds
(Rus)
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