The overall efficiency of the compressor is dependent on the design of both the impeller and diffuser. The vane diffuser reduces the operating range. However, by proper setting of the diffuser with reference to impeller, it is possible to achieve a good stage performance. This study is on the experimental investigation of the detailed flow behavior inside a centrifugal compressor stage for three different setting angles of the vane diffuser with reference to the fixed impeller blade outlet angle. It is seen that diffuser setting angles lower than the impeller outlet flow angle gives higher stage efficiency as well as flow range
Dr. Basharat Salim Associate Professor (Basharat@ksu.edu.sa ) Department of Mechanical Engineering C...
In the current research work, a computational analysis of a high-speed centrifugal compressor stage...
It is well recognised that the volute plays a important role on the stage performance of a turbo m...
This paper describes the behavior of steady and unsteady flow inside a centrifugal compressor stage....
The objective of this investigation was to compare the effects of two different diffuser vane geomet...
As centrifugal compressors find a huge number of applications in industry and in aeroengines, the de...
In this paper a three dimensional viscous flow field in a Centrifugal Impeller with backswept and le...
In this paper a three dimensional viscous flow field in a Centrifugal Impeller with backswept and le...
In a Centrifugal Compressor the work is imparted on the impeller to get higher total pressure of the...
As aviation fuel costs and consumption have continued to rise over recent decades, gas turbine engin...
An investigation of steady and unsteady flow phenomena in centrifugal compressors has been performed...
The centrifugal compressor for a marine use turbocharger with its design pressure ratio of 3.2 was t...
This research program focuses on characterizing the effect of impeller-diffuser interactions in a ce...
788-796This study establishes effectiveness of vaned diffuser in comparison with vaneless diffusers ...
In this paper the transonic flow field in a vaned diffuser of a contrifugal compressor has been stud...
Dr. Basharat Salim Associate Professor (Basharat@ksu.edu.sa ) Department of Mechanical Engineering C...
In the current research work, a computational analysis of a high-speed centrifugal compressor stage...
It is well recognised that the volute plays a important role on the stage performance of a turbo m...
This paper describes the behavior of steady and unsteady flow inside a centrifugal compressor stage....
The objective of this investigation was to compare the effects of two different diffuser vane geomet...
As centrifugal compressors find a huge number of applications in industry and in aeroengines, the de...
In this paper a three dimensional viscous flow field in a Centrifugal Impeller with backswept and le...
In this paper a three dimensional viscous flow field in a Centrifugal Impeller with backswept and le...
In a Centrifugal Compressor the work is imparted on the impeller to get higher total pressure of the...
As aviation fuel costs and consumption have continued to rise over recent decades, gas turbine engin...
An investigation of steady and unsteady flow phenomena in centrifugal compressors has been performed...
The centrifugal compressor for a marine use turbocharger with its design pressure ratio of 3.2 was t...
This research program focuses on characterizing the effect of impeller-diffuser interactions in a ce...
788-796This study establishes effectiveness of vaned diffuser in comparison with vaneless diffusers ...
In this paper the transonic flow field in a vaned diffuser of a contrifugal compressor has been stud...
Dr. Basharat Salim Associate Professor (Basharat@ksu.edu.sa ) Department of Mechanical Engineering C...
In the current research work, a computational analysis of a high-speed centrifugal compressor stage...
It is well recognised that the volute plays a important role on the stage performance of a turbo m...