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
combustion chamber
deformation
design
efficiency
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
Шорин, В. П.
Issue
Section
Title
File
Vol 12, No 1 (2013)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Test rig for a hydraulic drive under switched inertance control
(Rus)
Vol 5, No 1 (2006)
TECHNICAL SCIENCES
Mathematical modeling of hydrodynamic processes in a pipeline partially filled with air
(Rus)
Vol 5, No 1 (2006)
TECHNICAL SCIENCES
Algorithm of calculating hydrodynamic parameters of a pipeline partially filled with air
(Rus)
Vol 10, No 3-1 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
About the probes for measuring pulsations of pressure in the flowing part gas turbine engines
(Rus)
Vol 11, No 1 (2012)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Finite element techniques for pipe system vibroacoustical characteristics modelling
(Rus)
Vol 11, No 3-2 (2012): Special Issue
CONFERENCE MATERIALS
On the development of probes for measuring pressure pulsations in the gas-dynamic channel gas generator
(Rus)
Vol 1, No 1 (2002)
TECHNICAL SCIENCES
Design of a laser system of visualization of cavitational processes on an input of a pump of high power engines
(Rus)
Vol 2, No 1 (2003)
TECHNICAL SCIENCES
DIGITAL SPECKLE INTERFEROMETER FOR THE INVESTIGATION OF VIBRATION CHARACTERISTICS OF OBJECTS EXCITED SIMULTANEOUSLY AT SEVERAL FREQUENCIES
(Rus)
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