Improvement of characteristics of the ring input device of the aviation power plant with the screwfanter
The article considers the method of improving the characteristics of the ring inlet device, taking into account the influence of the propeller of an aircraft power plant with a turboprop engine. It is shown that increasing the total pressure loss in the inlet device by 5% increases, approximately, t...
Guardado en:
Autores principales: | Олег Володимирович Жорник, Ігор Федорович Кравченко, Михайло Михайлович Мітрахович |
---|---|
Formato: | article |
Lenguaje: | EN RU UK |
Publicado: |
National Aerospace University «Kharkiv Aviation Institute»
2021
|
Materias: | |
Acceso en línea: | https://doaj.org/article/417b15d927424c6f91b8729f6a0a3904 |
Etiquetas: |
Agregar Etiqueta
Sin Etiquetas, Sea el primero en etiquetar este registro!
|
Ejemplares similares
-
Substantiation of a turbulent viscosity model for studying the characteristics of a coaxial propfan and input device of a gas turbine engine
por: Олег Володимирович Жорник, et al.
Publicado: (2021) -
Flow simulation in a coaxial fan with boundary layer control
por: Вячеслав Юрійович Усенко, et al.
Publicado: (2021) -
Performance assessment of the ducted propfan of the turbofan engine with ultra-high bypass ratio
por: Олеся Валеріївна Денисюк
Publicado: (2021) -
Simulation of flow in a tandem fan of a turbofan engine
por: Антон Валерьевич Балалаев, et al.
Publicado: (2021) -
Selection of suppliers for the manufacture of high-technological products considering long logistic cargo delivery chains selecting suppliers
por: Олег Євгенович Федорович, et al.
Publicado: (2021)