Results 1 to 4 of about 4 (4)

Influence of temperature drop on the pressure rise in the fan circuit of the gas turbine engine turbo-fan attachment

Авіаційно-космічна техніка та технологія, 2023
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
Roman Maiboroda
doaj   +1 more source

Analysis of the influence of the nacelle on the thrust force of the fan circuit of the turbo-fan attachment

Авіаційно-космічна техніка та технологія, 2023
The subject of this study is the interaction between the engine nacelle of a three-circuit turbojet engine and a turbofan attachment. The object of this research is a model of a cylindrical engine nacelle and a fan part of the impeller of a turbofan ...
Roman Maiboroda
doaj   +1 more source

The influence of blade row temperature on the aerodynamic characteristics of an axial compressor impeller

Авіаційно-космічна техніка та технологія
The subject of this study was the characteristics of the compressor impeller regarding the heating of the blade row. The object of this study was the blade row of an axial compressor impeller.
Volodymyr Otroshchenko, Maryna Pikul, Yuriy Tereshchenko   +2 more
doaj   +1 more source

The influence of blade temperature on the aerodynamic characteristics of the profile

Авіаційно-космічна техніка та технологія
The subject of the study is the aerodynamic characteristics of the compressor blade concerning the effect of its surface thermal heating. The object of this study is the compressor grid of an axial compressor impeller.
Volodymyr Otroshchenko, Maryna Pikul
doaj   +1 more source