AbstractThere are presented calculating study of characteristics (loss factor and the lag angle of flow) of variable guide vane blade system for high pressure stage of centrifugal compressor with the influence of blades rotation angles (attack angle). The results are obtained using the known dependencies and using the calculation of viscous flow with ANSYS CFX and they are analyzed
Variable inlet guide vane (VIGV) is used to control the mass flow and generate prewhirl in centrifug...
Industrial centrifugal air compressors can require a combination of a large range of mass flow, high...
This paper describes a new universal algebraic model for the estimation of flow deflection and losse...
AbstractThere are presented calculating study of characteristics (loss factor and the lag angle of f...
AbstractExperimental data analysis for testing centrifugal compressor stage on control modes by the ...
This study reconstructed the flow field of a symmetrical variable inlet guide vane in a centrifugal ...
Variable inlet guide vanes (VIGVs) are most commonly used as the major control unit of integrally ge...
AbstractExperimental data analysis for testing centrifugal compressor stage on control modes by the ...
Variable inlet guide vanes (VIGVs) are widely used for flow throttling and also extending the operat...
The onset of aerodynamic instabilities in proximity of the left margin of the operating curve repres...
The blade angle distribution from the inlet to outlet of an impeller in a centrifugal compressor is ...
The modern engine has the requirement of high pressure ratio compressors. High diffusion blades are ...
The onset of aerodynamic instabilities in proximity of the left margin of the operating curve repres...
Purpose: the purpose of this work is to investigate the total pressure losses in the input guide van...
The performance of an automotive turbocharger centrifugal compressor has been studied by developing ...
Variable inlet guide vane (VIGV) is used to control the mass flow and generate prewhirl in centrifug...
Industrial centrifugal air compressors can require a combination of a large range of mass flow, high...
This paper describes a new universal algebraic model for the estimation of flow deflection and losse...
AbstractThere are presented calculating study of characteristics (loss factor and the lag angle of f...
AbstractExperimental data analysis for testing centrifugal compressor stage on control modes by the ...
This study reconstructed the flow field of a symmetrical variable inlet guide vane in a centrifugal ...
Variable inlet guide vanes (VIGVs) are most commonly used as the major control unit of integrally ge...
AbstractExperimental data analysis for testing centrifugal compressor stage on control modes by the ...
Variable inlet guide vanes (VIGVs) are widely used for flow throttling and also extending the operat...
The onset of aerodynamic instabilities in proximity of the left margin of the operating curve repres...
The blade angle distribution from the inlet to outlet of an impeller in a centrifugal compressor is ...
The modern engine has the requirement of high pressure ratio compressors. High diffusion blades are ...
The onset of aerodynamic instabilities in proximity of the left margin of the operating curve repres...
Purpose: the purpose of this work is to investigate the total pressure losses in the input guide van...
The performance of an automotive turbocharger centrifugal compressor has been studied by developing ...
Variable inlet guide vane (VIGV) is used to control the mass flow and generate prewhirl in centrifug...
Industrial centrifugal air compressors can require a combination of a large range of mass flow, high...
This paper describes a new universal algebraic model for the estimation of flow deflection and losse...