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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endurance limit
experiment
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gas turbine engine
mathematical model
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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
Попов, И. П.
Issue
Section
Title
File
Vol 5, No 1 (2006)
TECHNICAL SCIENCES
Investigating the process of shaping solid moulded parts according to the outward happing-moulding pattern
(Rus)
Vol 5, No 2-1 (2006): Special Issue
TECHNICAL SCIENCES
The analysis of the crimp seal-forming process in the LS–DYNA system
(Rus)
Vol 5, No 2-1 (2006): Special Issue
TECHNICAL SCIENCES
The determination of optimal characteristics of technologic processes of production
(Rus)
Vol 6, No 1 (2007)
TECHNICAL SCIENCES
Inereasing limit coefficient of thin material drawing in a die with an elastic element (holder)
(Rus)
Vol 9, No 4 (2010)
AIRCRAFT AND SPACE ROCKET ENGINEERING
Forming parts of the “atomizer” type for aircraft engines
(Rus)
Vol 13, No 1 (2014)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Computer simulation of forming thin-walled t-tees
(Rus)
Vol 11, No 1 (2012)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Method of producing thin-walled conical parts in a die with an elastic element
(Rus)
Vol 11, No 2 (2012)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Application of a casting technique in the form of piston pressing for grinding the structure of an aluminum alloy
(Rus)
Vol 11, No 5-2 (2012): Special Issue
CONFERENCE MATERIALS
Research of possibilities to obtain high-alloy aluminummagnesium alloys
(Rus)
Vol 11, No 5-2 (2012): Special Issue
CONFERENCE MATERIALS
Method of plastic structure formation
(Rus)
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