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
Nozhnitsky, Yu. A.
Issue
Section
Title
File
Vol 10, No 3-1 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Methodical features of vibration tests of rotating blades using dynamic spin rigs
(Rus)
Vol 14, No 3-1 (2015): Special Issue
ISSUE WITHOUT SECTION
Requirements for the order and the procedure of estimating structural strength characteristics of metal alloys for the main and critical parts of aviation gas turbine engines
(Rus)
Vol 14, No 3-1 (2015): Special Issue
ISSUE WITHOUT SECTION
New possibilities of using spin rigs to provide gas turbine engine strength reliability
(Rus)
Vol 14, No 3-1 (2015): Special Issue
ISSUE WITHOUT SECTION
Experimental determination of thermal-fatigue life of turbine blades with various coatings made of an advanced heat resistant nickel alloy
(Rus)
Vol 17, No 3 (2018)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Mechanical engineer, scientist, teacher. On the occasion of centenary of the birth of I.A. Birger
(Rus)
Vol 18, No 3 (2019)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Prospects of application of additive technologies to develop parts and components of gas turbine engines and ramjets
(Rus)
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