VESTNIK of Samara University.
Aerospace and Mechanical Engineering
ISSN 2542-0453 (Print)
ISSN 2541-7533 (Online)
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Combustion chamber
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Combustion chamber
Gas turbine engine
Mathematical model
Spacecraft
algorithm
blade
combustion chamber
design
efficiency
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
Болотов, М. А., Самарский государственный аэрокосмический университет имени академика С.П. Королёва (национальный исследовательский университет), Russian Federation
Issue
Section
Title
File
Vol 10, No 2 (2011)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Research of errors of measuring angular location parameters of holes in turbine and compressor discs of gas turbine engines
(Rus)
Vol 10, No 2 (2011)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Models and methods of optimizing the procedure of measuring gas turbine engine parts using coordinate measuring devices
(Rus)
Vol 11, No 3-2 (2012): Special Issue
CONFERENCE MATERIALS
Technological processes simulation incomplex parts production of aerospacetechnical equipment: problems and the ways of their solving
(Rus)
Vol 11, No 3-2 (2012): Special Issue
CONFERENCE MATERIALS
NC machine tools contact measuring devices uncertainty when products geometrical parameters control
(Rus)
Vol 11, No 3-3 (2012): Special Issue
CONFERENCE MATERIALS
Dimensions of controlled on CMM flat surfaces as an influencing factor of their coordinate-positional parameters measurement errors
(Rus)
Vol 11, No 5-2 (2012): Special Issue
CONFERENCE MATERIALS
Research of technological heredity influence on setting of procedure of measurements on coordinate-measurement machine in case of out-of-flatness detecting for aircraft engineering parts
(Rus)
Vol 13, No 5-3 (2014): Special Issue
ISSUE WITHOUT SECTION
Development of methods of carrying out experimental research of measurement errors for sets of geometrical parameters on NC equipment as in the case of a turbine disk
(Rus)
Vol 13, No 5-3 (2014): Special Issue
ISSUE WITHOUT SECTION
Improving the accuracy of assessing the position deviation in coordinate measurements of GTE compressor and turbine blade profiles
(Rus)
Vol 14, No 3-2 (2015): Special Issue
ISSUE WITHOUT SECTION
Comparative research of algorithms of measuring the geometry of complex profiles of gas turbine engine compressor blades
(Rus)
Vol 15, No 2 (2016)
MECHANICAL ENGINEERING AND POWER ENGINEERING
Study of uncertainty of measuring geometrical parameters of gas turbine engine compressor blade profiles
(Rus)
Vol 10, No 3-3 (2011): Special Issue
AIRCRAFT AND SPACE ROCKET ENGINEERING
Measurment procedure optimizing geometrical parameters of measure GTE feature on coordinate measuring machine
(Rus)
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