Influence of temperature drop on the pressure rise in the fan circuit of the gas turbine engine turbo-fan attachment
The subject of this study is the working process in a turbofan attachment of a gas turbine engine. The object of study is the fan part of the impeller of a turbofan attachment. The aim of this study was to evaluate the effect of temperature difference in a two-tier impeller on the degree of pressure...
Main Author: | Roman Maiboroda |
---|---|
Format: | Article |
Language: | English |
Published: |
National Aerospace University «Kharkiv Aviation Institute»
2023-08-01
|
Series: | Авіаційно-космічна техніка та технологія |
Subjects: | |
Online Access: | http://nti.khai.edu/ojs/index.php/aktt/article/view/2071 |
Similar Items
-
Analysis of the influence of the nacelle on the thrust force of the fan circuit of the turbo-fan attachment
by: Roman Maiboroda
Published: (2023-08-01) -
Simulation of flow in a tandem fan of a turbofan engine
by: Антон Валерьевич Балалаев, et al.
Published: (2021-08-01) -
EFFECT OF THE SOLIDITY ON THE AERODYNAMIC LOADING OF THE AXIAL FAN
by: Екатерина Викторовна Дорошенко, et al.
Published: (2020-08-01) -
Performance assessment of the ducted propfan of the turbofan engine with ultra-high bypass ratio
by: Олеся Валеріївна Денисюк
Published: (2021-08-01) -
Control laws of an aviation gas turbine engine with a turbofan additional unit
by: Serhii Tovkach
Published: (2023-08-01)