The paper describes the results of an experimental campaign performed on a three bladed axial inducer with tapered hub and variable pitch, named RAPDUD. The tests have been performed at the Cavitating Pump Rotordynamic Test Facility at Sitael. S.p.A. under similarity conditions. The tests aimed at characterizing the flow instabilities arising in the fluid elaborated by the inducer at different flow coefficients through two reference frames: a statoric frame by placing pressure transducers on the casing and a rotoric frame by placing the transducers on the inducer hub. The additional reference frame has allowed a better understanding of the flow phenomena arising inside the inducer
The present paper illustrates the results of recent experiments carried out under ESA funding in the...
The present paper illustrates the results of recent experiments carried out under ESA funding in the...
The effects of thermal cavitation on the flow instabilities developing in a three-bladed, tapered-hu...
The present paper illustrates the main results of an experimental campaign conducted using the CPRTF...
The paper presents the results of the experimental activity carried out in the CPRTF (Cavitating Pum...
The paper describes the results of recent experiments carried out in the Cavitating Pump Rotordynami...
The present paper reports the experimental characterization of the cavitation induced flow instabili...
A high-head three-bladed inducer has been equipped with pressure taps along the blade channels to ch...
The present paper illustrates the results of recent experiments carried out under ESA funding in the...
The present paper illustrates the results of recent experiments carried out under ESA funding in the...
International audienceThe paper describes results of recent experiments carried out under similarity...
The paper illustrates and compares the results of the experimental campaigns carried out in the Cavi...
The present paper illustrates the main results of an experimental campaign conducted using the CPRTF...
Turbopumps is a key component of the feeding system for high thrust, liquid rocket engines such as t...
The paper illustrates the main results of an experimental campaign conducted in the CPRTF (Cavitatin...
The present paper illustrates the results of recent experiments carried out under ESA funding in the...
The present paper illustrates the results of recent experiments carried out under ESA funding in the...
The effects of thermal cavitation on the flow instabilities developing in a three-bladed, tapered-hu...
The present paper illustrates the main results of an experimental campaign conducted using the CPRTF...
The paper presents the results of the experimental activity carried out in the CPRTF (Cavitating Pum...
The paper describes the results of recent experiments carried out in the Cavitating Pump Rotordynami...
The present paper reports the experimental characterization of the cavitation induced flow instabili...
A high-head three-bladed inducer has been equipped with pressure taps along the blade channels to ch...
The present paper illustrates the results of recent experiments carried out under ESA funding in the...
The present paper illustrates the results of recent experiments carried out under ESA funding in the...
International audienceThe paper describes results of recent experiments carried out under similarity...
The paper illustrates and compares the results of the experimental campaigns carried out in the Cavi...
The present paper illustrates the main results of an experimental campaign conducted using the CPRTF...
Turbopumps is a key component of the feeding system for high thrust, liquid rocket engines such as t...
The paper illustrates the main results of an experimental campaign conducted in the CPRTF (Cavitatin...
The present paper illustrates the results of recent experiments carried out under ESA funding in the...
The present paper illustrates the results of recent experiments carried out under ESA funding in the...
The effects of thermal cavitation on the flow instabilities developing in a three-bladed, tapered-hu...