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
efficiency
endurance limit
experiment
finite element method
gas turbine engine
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mathematical modeling
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Keywords
Combustion chamber
Gas turbine engine
Mathematical model
Spacecraft
algorithm
blade
combustion chamber
efficiency
endurance limit
experiment
finite element method
gas turbine engine
mathematical model
mathematical modeling
modeling
optimization
residual stresses
simulation
spacecraft
structure
turbine
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Author Details
Author Details
Хаймович, А. И., Самарский государственный аэрокосмический университет имени академика С.П. Королёва (национальный исследовательский университет), Russian Federation
Issue
Section
Title
File
Vol 12, No 4 (2013)
ISSUE WITHOUT SECTION
Assessing the strain-stress state parameters of cutting tools and parts during machining
(Rus)
Vol 5, No 3 (2006)
TECHNICAL SCIENCES
Improving industrial organization at amachinery construction plant on the basis of reengineering
(Rus)
Vol 7, No 1 (2008)
CONTROL, COMPUTER SCIENCE AND INFORMATION SCIENCE
Procedure rules of press forging business process development and coordination
(Rus)
Vol 9, No 4 (2010)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Experimental definition of the optimum scheme of shaping forged impellers by high-speed forging
(Rus)
Vol 10, No 1 (2011)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Optimization of thermomechanical parameters of high speed forging of titanium alloys
(Rus)
Vol 11, No 3-2 (2012): Special Issue
CONFERENCE MATERIALS
Method of compressor blades life gaining processed by high speed forging from α+β titanium alloys with heating above a point of polymorphic transormations
(Rus)
Vol 11, No 5-2 (2012): Special Issue
CONFERENCE MATERIALS
Analysis оf the cutting force of heat resisting alloys during high-speed milling
(Rus)
Vol 13, No 5-3 (2014): Special Issue
ISSUE WITHOUT SECTION
Research of machinability of heat resistant steels 10Х11НN23T3MР-ВД used in parts of gas turbine engines
(Rus)
Vol 14, No 3-2 (2015): Special Issue
ISSUE WITHOUT SECTION
Formation of a model of rheological properties of hard-to-machine materials in the process of intensive cutting force deflection
(Rus)
Vol 10, No 3-3 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
The phenomenological models of the dynamic recrystallization of alloys for aviation
(Rus)
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