Aerospace Technic and Technology
Keywords
additive technologies
aircraft
aircraft engine
climate
cooling
corrosion
efficiency
finite element method
gas turbine engine
gas turbine unit
heat load
mathematical model
microstructure
modeling
numerical experiment
numerical simulation
optimization
power plant
quality
spacecraft
strength
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Дуаиссиа, Омар Хадж Аисcа, Ukraine
No 6 (2018): Aerospace technic and technology
- Engines and power plants of aircraft
FEATURES OF HEAT TRANSFER IN THE GAS TURBINE ENGINE BEARING CHAMBER
Abstract
PDF (Русский)
ISSN: 2663-2217