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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endurance limit
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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
Ivashin, P. V.
Issue
Section
Title
File
Vol 12, No 3-1 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Interconnection of propagation velocity and electrical conductivity of flame in ICEs
(Rus)
Vol 12, No 2 (2013)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Flame propagation velocity and ionization in burning gasoline and methane with addition of hydrogen
(Rus)
Vol 12, No 3-2 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Evaluation of internal combustion engine cycle work using an ionic current sensor
(Rus)
Vol 12, No 3-2 (2013): Vestnik SSAU
ISSUE WITHOUT SECTION
Adhesion strength of heat-insulating and wear-resistant ceramic coatings on aluminum alloys
(Rus)
Vol 11, No 3-3 (2012): Special Issue
CONFERENCE MATERIALS
The application of technology microarc oxidation to repair and restore characteristics of products from aluminum alloy AK9
(Rus)
Vol 10, No 5 (2011)
ISSUE WITHOUT SECTION
Using an ionization probe removed from the sparking plug for the development of a two-zone ICE combustion model
(Rus)
Vol 10, No 5 (2011)
ISSUE WITHOUT SECTION
Primary assessment of the effects of temperature drop on the mechanical properties of a protective oxide layer obtained by microarc oxidation on alloy AK9
(Rus)
Vol 15, No 3 (2016)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Using the phenomenon of electrical conduction of flame of non-homogeneous air-fuel mixture in design and development of combustion chamber
(Rus)
Vol 10, No 3-2 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Application of technology microarc oxidation (mao) aluminum and titanium alloys to improve performance parts in engines
(Rus)
Vol 10, No 3-3 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Application of flame electro conductivity for combustion analysis in spark ignition ICE
(Rus)
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