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
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
Косицын, И. П.
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Vol 5, No 2-1 (2006): Special Issue
TECHNICAL SCIENCES
The application loop labyrinth seals (LLS) for increasing effect of automatic unload bearings system (AUBS) turbopumps
(Rus)
Vol 5, No 2-1 (2006): Special Issue
TECHNICAL SCIENCES
Results of experimental tests of «dry» seals for NK-37 gas turвine separate compressor with the use of air as working body
(Rus)
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