788-796This study establishes effectiveness of vaned diffuser in comparison with vaneless diffusers in centrifugal compressor. Hot wire measurements at three inter-vane positions for mean velocity, turbulent kinetic energy and flow angle distributions in vaneless space and vane region of a low speed centrifugal compressor are presented. A low speed compressor with a 19 bladed backswept impeller and 16-wedge vanes diffuser was used. The flow entering diffuser closely resembles classic jet-wake flow characteristic of centrifugal impeller discharges. A strong upstream influence of diffuser vanes, which resulted in significant variations in flow quantities between vane-to-vane locations, was observed. Circumferential variations due to pass...
International audienceExperimental investigation of mean flow velocity and pressure inside the vane...
Vaneless diffuser rotating stall is a major problem for centrifugal compressors since it is a limit ...
The centrifugal compressor for a marine use turbocharger with its design pressure ratio of 3.2 was t...
In a Centrifugal Compressor the work is imparted on the impeller to get higher total pressure of the...
An investigation of steady and unsteady flow phenomena in centrifugal compressors has been performed...
The objective of this investigation was to compare the effects of two different diffuser vane geomet...
The overall efficiency of the compressor is dependent on the design of both the impeller and diffuse...
348-354Flow computations have been performed in vaneless diffuser (diam, 1 m), in low speed backswep...
As centrifugal compressors find a huge number of applications in industry and in aeroengines, the de...
The flow field development in vaneless and vaned diffuser of a transonic centrifugal compressors has...
Parameters of flow are calculated in vaneless diffusers with relative width 0,014–0,10. Inlet angles...
The effect of the width of the vaneless diffuser on the stage performance and flow fields of a centr...
To investigate the influence of the vaneless space between impeller exit and the diffuser vanes, det...
This paper presents the performance of a conventional turbocharger centrifugal compressor with a van...
This paper presents the performance of a conventional turbocharger centrifugal compressor with a van...
International audienceExperimental investigation of mean flow velocity and pressure inside the vane...
Vaneless diffuser rotating stall is a major problem for centrifugal compressors since it is a limit ...
The centrifugal compressor for a marine use turbocharger with its design pressure ratio of 3.2 was t...
In a Centrifugal Compressor the work is imparted on the impeller to get higher total pressure of the...
An investigation of steady and unsteady flow phenomena in centrifugal compressors has been performed...
The objective of this investigation was to compare the effects of two different diffuser vane geomet...
The overall efficiency of the compressor is dependent on the design of both the impeller and diffuse...
348-354Flow computations have been performed in vaneless diffuser (diam, 1 m), in low speed backswep...
As centrifugal compressors find a huge number of applications in industry and in aeroengines, the de...
The flow field development in vaneless and vaned diffuser of a transonic centrifugal compressors has...
Parameters of flow are calculated in vaneless diffusers with relative width 0,014–0,10. Inlet angles...
The effect of the width of the vaneless diffuser on the stage performance and flow fields of a centr...
To investigate the influence of the vaneless space between impeller exit and the diffuser vanes, det...
This paper presents the performance of a conventional turbocharger centrifugal compressor with a van...
This paper presents the performance of a conventional turbocharger centrifugal compressor with a van...
International audienceExperimental investigation of mean flow velocity and pressure inside the vane...
Vaneless diffuser rotating stall is a major problem for centrifugal compressors since it is a limit ...
The centrifugal compressor for a marine use turbocharger with its design pressure ratio of 3.2 was t...