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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Spacecraft
algorithm
blade
combustion chamber
deformation
design
efficiency
endurance limit
experiment
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gas turbine engine
mathematical model
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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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Author Details
Author Details
Гафуров, С. А.
Issue
Section
Title
File
Vol 13, No 1 (2014)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Calculation of hydrodynamic noise in the diffuser of a pulsation damper flow channel
(Rus)
Vol 11, No 2 (2012)
MECHANICAL ENGINEERING AND POWER ENGINEERING
The influence of a combined pump’s auger-centrifugal stage inlet design on its vibration and pulsation states
(Rus)
Vol 11, No 2 (2012)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Analysis of the causes of auger-centrifugal pump bearing destruction
(Rus)
Vol 11, No 3-2 (2012): Special Issue
CONFERENCE MATERIALS
CFD modeling of air penetration into the fuel supply pipeline
(Rus)
Vol 11, No 3-2 (2012): Special Issue
CONFERENCE MATERIALS
Investigation of the causes of the auger-centrifugal pump bearing destruction
(Rus)
Vol 10, No 5 (2011)
ISSUE WITHOUT SECTION
Analysis estimation of pulse jet engine operation in detonation mode
(Rus)
Vol 10, No 3-4 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Development of numerical models of working process in fuel auger-centrifugal pump
(Rus)
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