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
Тихомирова, Е. А.
Issue
Section
Title
File
Vol 8, No 3-3 (2009): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Selection of new heat-resistant nickel alloys for advanced aviation engines
(Rus)
Vol 11, No 3-1 (2012): Special Issue
CONFERENCE MATERIALS
The new testung method of coatings on high-temperature alloys
(Rus)
Vol 11, No 3-1 (2012): Special Issue
CONFERENCE MATERIALS
Instrument to measure material resistance to thermo-mechanical fatigue
(Rus)
Vol 13, No 5-2 (2014): Special Issue
ISSUE WITHOUT SECTION
The influence of maximum temperature of heating on the thermal fatigue of nickel heat-resistant alloys under thermocyclic tests
(Rus)
Vol 13, No 5-3 (2014): Special Issue
ISSUE WITHOUT SECTION
Analysis of the results of thermal cycic tests using TC-maps and problems of investigating thermal fatigue of materials
(Rus)
Vol 10, No 3-2 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
On the issue of research of the properties of the heat-resistant nickel single-crystal superalloys
(Rus)
Vol 10, No 3-3 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
The Laue back-reflection method for determination orientation and subgrains disorientation of blade manufacture single-crystal pieces
(Rus)
Vol 10, No 3-3 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
About investigations the orientation dependence of single-crystal turbine blade exploitation properties
(Rus)
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